Impact of acoustic Doppler current profiler (ADCP) motion on structure function estimates of turbulent kinetic energy dissipation rate

Abstract

Turbulent mixing is a key process in the transport of heat, salt, and nutrients in the marine environment, with fluxes commonly derived directly from estimates of the turbulent kinetic energy dissipation rate, $\mathit{\epsilon }$. Time series of $\mathit{\epsilon }$ estimates are therefore useful in helping to identify and quantify key biogeochemical processes. The velocity structure function method can be used to determine time series of $\mathit{\epsilon }$ estimates using along-beam velocity measurements from suitably configured acoustic Doppler current profilers (ADCPs). Shear in the background current can bias such estimates; therefore, standard practice is to deduct the mean or linear trend from the along-beam velocity over the period of an observation burst. This procedure is effective if the orientation of the ADCP to the current remains constant over the burst period. However, if the orientation of the ADCP varies, a proportion of the velocity difference between bins is retained in the structure function and the resulting $\mathit{\epsilon }$ estimates will be biased. Long-term observations from a mooring with three inline ADCPs show the heading oscillating with an angular range that depends on the flow speed: from large, slow oscillations at low flow speeds to smaller, higher-frequency oscillations at higher flow speeds. The mean tilt was also determined by the flow speed, whilst the tilt oscillation range was primarily determined by surface wave height. Synthesised along-beam velocity data for an ADCP subject to sinusoidal oscillation in a sheared flow indicate that the retained proportion of the potential bias is primarily determined by the angular range of the oscillation, with the impact varying between beams depending on the mean heading relative to the flow. Since the heading is typically unconstrained in a tethered mooring, heading oscillation is likely to be the most significant influence on the retained bias for a given level of shear. Use of an instrument housing designed to reduce oscillation would mitigate the impact, whilst if the shear is linear over the observation depth range, the bias can be corrected using a modified structure function method designed to correct for bias due to surface waves.

1 Introduction

The most well-established technique for making observations of the turbulent kinetic energy (TKE) dissipation rate, $\mathit{\epsilon }$, uses shear microstructure profilers e.g.. The approach produces high-resolution vertical profiles of $\mathit{\epsilon }$ but is expensive as it requires a surface vessel and staff, as well as being limited in the sampling interval achievable, the duration of the observations, and the conditions under which they can be made. These limitations are partially addressed by mounting the shear probes on buoyancy-controlled gliders, although deployment periods remain limited (typically between 1 and 3 weeks) and remote updating of instructions is typically required when the glider periodically surfaces e.g. to correct for advection . An alternative approach using acoustic Doppler velocimeters (ADVs) to make point observations of the velocity spectrum has been used from a mooring, but $\mathit{\epsilon }$ estimates are subject to potentially high levels of motion-induced contamination .

In comparison, the velocity structure function method offers the potential to generate time series of turbulence parameters using industry-standard acoustic Doppler current profiler (ADCP) instruments, which are relatively cheap, robust, and designed for long-term deployment under the widest range of environmental conditions.

Standard ADCPs have three or four beams, each oriented at a common beam angle to the instrument axis so that if the instrument is nearly vertical, the velocity field can then be determined . Improvements in the accuracy of the velocity measurements allowed ADCPs to be used to generate time series estimates of the rate of production of TKE , although the presence of surface waves and instrument motion results in significant biases, limiting applicability. used a modified design with a single beam oriented along the instrument axis to make direct measurement of the vertical velocity in order to measure turbulence parameters, and this has been incorporated in recent instrument designs with an additional beam, providing enhanced functionality .

The structure function method for estimating $\mathit{\epsilon }$ derives from the Kolmogorov hypotheses of similarity and local isotropy in high-Reynolds-number flows translated from the original 1941 Russian publications. Originally used for observations of atmospheric turbulence, the technique is now established as a means of acquiring long-term observations of $\mathit{\epsilon }$ in the aquatic environment under a wide range of conditions e.g..

The method determines $\mathit{\epsilon }$ as a function of the difference in the along-axis turbulent velocity with the spatial separation of the observation points. This is readily applied to ADCPs, which by design measure the radial (along-beam) velocity at defined separation distances. The detection limit and resolution are inherently determined by the uncertainty of the velocity measurements, which depend on manufacturers' proprietary techniques and are not published in a consistent form. However, the development of new ADCP operating modes such as pulse–pulse coherent and high ping rates has allowed high-spatial-resolution low-variance velocity measurements to be made without the need for extensive time averaging, but with limited beam range. This has encouraged innovations such as deployments on tethered moorings to acquire turbulence measurements in sections of the water column important for mixing e.g. and on surface drifters to provide quasi-synoptic observations of the spatial distribution of turbulence e.g..

Standard practice is to assume that any non-turbulent velocity differences between bins are static or slowly varying such that they can be excluded by deducting the mean or linear trend over a burst of profiles for each bin . It is then assumed that all residual velocity differences are turbulent.

Shear in the background flow is a potential source of non-turbulent velocity differences between bins for standard ADCP angled beams. If the ADCP is on a static bed frame, the orientation of the beams to the background flow will be constant over the burst period, and the standard procedure will fully remove the non-turbulent velocity difference between bins due to the sheared flow. Similarly, for a static vertical beam, the along-beam velocity is independent of any shear in the background flow; therefore, no velocity difference between bins arises.

However, an ADCP on a tethered mooring is typically free to rotate about its vertical axis so that the heading varies. Drag on the mooring and the instrument may also result in the instrument tilt varying, resulting in differences in the vertical range and the orientation of the beams, whilst surface waves may affect the instruments directly or by varying the tension and shape of the mooring. Similarly, ADCPs deployed on surface drifters are free to rotate about their vertical axis, whilst surface waves may cause periodic variation in the instrument tilt.

Velocities due to the rotation of a tethered or drifter-mounted ADCP are normal to the beams (both angled and vertical) and therefore do not directly contribute to the observed along-beam velocities . However, changes in the ADCP orientation will result in a variation in the background flow contribution to the along-beam velocity, with angled beams affected by changes in both heading and tilt, whilst vertical beams will only be affected by changes in tilt. The magnitude of the background flow contribution to the along-beam velocity increases as the beam becomes more closely aligned with the flow and vice versa. The burst mean will therefore underestimate the contribution for those profiles when the beam is most closely aligned with the background flow and overestimate it at other times. Deducting the burst mean cannot fully remove this time-varying contribution. If the flow is sheared, a proportion of the associated non-turbulent velocity difference between bins is unavoidably retained, contributing to the structure function and biassing the resulting $\mathit{\epsilon }$ estimates.

This is similar to the effect of the vertical gradient of the orbital velocity forced by surface gravity waves, which can lead to non-turbulent velocity differences between bins being retained in the structure function and potential bias in $\mathit{\epsilon }$ estimates .

The aims of this paper are to demonstrate that $\mathit{\epsilon }$ estimates derived from velocity observations from the angled beams of a tethered ADCP in a sheared flow using the standard structure function method are inherently susceptible to bias if the instrument orientation to the flow varies, to highlight the key factors determining the level of such bias, and to outline possible means of mitigating or correcting for the effect. The principles equally apply to the vertical beam of ADCPs subject to tilt such that the background flow contributes a periodic component to the along-beam velocity. Whilst the specific impact has not been evaluated, the same conclusions apply. Section  briefly outlines the structure function methodology and considers the scaling of the potential $\mathit{\epsilon }$ bias arising due to linear shear in the background flow. Section  describes observations from a mooring in the central Celtic Sea with three tethered ADCPs at different depths to illustrate how the motion of the ADCP varies with both the flow speed and the amplitude of surface waves. Section  uses synthetic data to examine the dependence on the level of retained $\mathit{\epsilon }$ bias on the ADCP motion. Finally, Sect.  is a discussion of the findings and the potential for correcting the bias.

Figure 1

Geometry for a Teledyne RDI WorkHorse four-beam ADCP. Solid red lines indicate the centre line for the beams, each with beam angle $\mathit{\theta }$ to the along-instrument $z$ axis (typically oriented vertically), with beams 1 and 2 symmetric about the $z$ axis in the $y=\mathrm{0}$ plane and beams 3 and 4 similarly oriented in the $x=\mathrm{0}$ plane. Bins $n$ to $n+\mathrm{4}$ are shown for each beam, with $\mathit{\delta }z$ being the bin centre separation distance along the $z$ axis and $\mathit{\delta }r=\mathit{\delta }z/\cos \mathit{\theta }$ being the along-beam bin centre separation distance. Heading, ${\mathit{\varphi }}_{\mathrm{H}}$, describes the compass angle for beam 3, pitch ${\mathit{\varphi }}_{\mathrm{P}}$ the rotation from vertical about the $x$ axis, and roll ${\mathit{\varphi }}_{\mathrm{R}}$ the rotation from vertical about the $y$ axis, with the sign convention dependent on whether the instrument is oriented upwards- or downwards-looking.

[Figure omitted. See PDF]

2 Potential bias

2.1 Structure function method

Figure  illustrates the geometry for a Teledyne RDI WorkHorse four-beam ADCP, which is similar to that for other instruments. Based on a standard Cartesian coordinate framework $(x,y,z)$ relative to the transducer head, each of the beams is tilted at beam angle $\mathit{\theta }$ to the along-instrument $z$ axis, with beams 1 and 2 oriented either side of the $z$ axis in the $y=\mathrm{0}$ plane and beams 3 and 4 similarly positioned in the $x=\mathrm{0}$ plane. Instrument orientation and motion can then be described in terms of heading (${\mathit{\varphi }}_{\mathrm{H}}$), pitch (${\mathit{\varphi }}_{\mathrm{P}}$), and roll (${\mathit{\varphi }}_{\mathrm{R}}$) as the rotation angles about the $z$, $x$, and $y$ axes, respectively. Along-beam velocities, $b$ (positive towards the transducer), are measured for volume bins centred at fixed distances (time range gates) from the transducer such that the $z$ coordinate is the same for bin $n$ in each beam. The $z$ axis separation distance between bin centres, $\mathit{\delta }z$, is the same for all beams and bins, with the along-beam separation distance between adjacent bins in any beam being $\mathit{\delta }r=\mathit{\delta }z/\cos \mathit{\theta }$.

By observing the along-beam velocities at fixed separation distances, ADCPs provide the information required for independent longitudinal structure function calculations for each beam. The theoretical basis of the method is described in detail elsewhere e.g.. Applied to a burst of ADCP observations comprising $N$ sets of along-beam velocity profiles, $b(i,j,k)$, where $i$ is the beam number, $j$ is the bin number, and $k$ is the profile number $(\mathrm{1}\le k\le N)$, the turbulent velocity, $b^{\prime }$, is typically calculated as

1$$b^{\prime }(i,j,k)=b(i,j,k)-⟨b(i,j)⟩,$$ with the angle brackets indicating the mean of $b(i,j)$ over the $N$ profiles in the burst . An alternative approach is to deduct the linear trend of $b$ over the burst, allowing for a steady variation in the speed of the background flow .

The second-order structure function, $D_{\mathrm{LL}}$, for along-beam separation distance $r_n=n\mathit{\delta }r$, where $n$ is the number of bins separating the observations, is then evaluated using a bin-centred difference scheme as 2$$D_{\mathrm{LL}}(i,j,r_n)=⟨{\left[b^{\prime }\left(i,j-\frac{n}{\mathrm{2}}\right)-b^{\prime }\left(i,j+\frac{n}{\mathrm{2}}\right)\right]}^{\mathrm{2}}⟩,$$ with the angle brackets again indicating the arithmetic mean across the $N$ profiles in the burst . For odd $n$, the mean of the two offset bin difference options is taken. This approach yields individual $D_{\mathrm{LL}}(i,j,r_n)$ values, allowing a vertical profile of $\mathit{\epsilon }$ estimates to be constructed e.g.. An alternative approach evaluates all possible $r_n$ for a range of bins to give a representative value for the depth range .

The Kolmogorov hypotheses anticipate that $D_{\mathrm{LL}}\left(r\right)$ should vary solely as a function of $\mathit{\epsilon }$ and $r$ as 3$$D_{\mathrm{LL}}\left(r\right)=C_{\mathrm{2}}{\mathit{\epsilon }}^{\frac{\mathrm{2}}{\mathrm{3}}}{r}^{\frac{\mathrm{2}}{\mathrm{3}}},$$ with $C_{\mathrm{2}}$ being an empirical constant, for which atmospheric studies suggest a value of $\mathrm{2.1}\pm \mathrm{0.1}$ , whilst laboratory measurements of grid turbulence in high-Reynolds-number flows give a value of $\mathrm{2.0}\pm \mathrm{15}$ % . The appropriate value is also potentially influenced by Reynolds number, anisotropy of the turbulent eddies, and proximity to a boundary . Studies commonly adopt values of 2.1 e.g. or 2.0 e.g..

Doppler noise associated with the velocity observations introduces an offset; hence, standard practice is to use a least-squares linear regression of $D_{\mathrm{LL}}$ against $r^{\frac{\mathrm{2}}{\mathrm{3}}}$ as 4$$D_{\mathrm{LL}}\left(r\right)=a_{\mathrm{0}}+a_{\mathrm{1}}{r}^{\frac{\mathrm{2}}{\mathrm{3}}},$$ with the intercept $a_{\mathrm{0}}$ typically being taken as twice the Doppler noise variance of the velocity measurements, although demonstrate a dependence on $\mathit{\epsilon }$ levels, with $a_{\mathrm{0}}$ decreasing with increasing $\mathit{\epsilon }$.

The gradient $a_{\mathrm{1}}$ from Eq. () is then used to determine $\mathit{\epsilon }$ as 5$$\mathit{\epsilon }={\left({\displaystyle \frac{a_{\mathrm{1}}}{C_{\mathrm{2}}}}\right)}^{\frac{\mathrm{3}}{\mathrm{2}}}.$$ The linear regression is evaluated for $r_n\le r_{\max }$, which is required to be less than the spatial scale over which the isotropic turbulence assumption in the Kolmogorov hypotheses is considered to be valid. In practice there may be a trade-off between limiting the spatial scale and increasing the number of data points to improve confidence in the linear regression.

describe a modified method to correct for the bias due to the spatial gradient of the orbital velocities associated with surface gravity waves. The periodic nature of the wave-forced contribution to the along-beam velocity, $\stackrel{\mathrm{̃}}{b}$, means that it is wholly retained in $b^{\prime }$. Over a limited spatial scale, the velocity difference between bins, $\mathit{\delta }\stackrel{\mathrm{̃}}{b}\left(r\right)$, varies approximately linearly with $r$; hence, the contribution to $D_{\mathrm{LL}}$ varies as $r^{\mathrm{2}}$. Modifying the regression in Eq. () with the inclusion of an additional term as 6$$D_{\mathrm{LL}}\left(r\right)=a_{\mathrm{0}}+a_{\mathrm{1}}{r}^{\frac{\mathrm{2}}{\mathrm{3}}}+a_{\mathrm{3}}(r^{\frac{\mathrm{2}}{\mathrm{3}}}{)}^{\mathrm{3}}$$ allows the turbulent contribution, described by $a_{\mathrm{1}}$, to be isolated from the non-turbulent component due to the wave orbital velocity.

2.2 Potential impact of shear

For an upward- or downward-looking ADCP with constant heading such that the horizontal projection of beam $i$ is oriented into a steady, non-turbulent, vertically sheared horizontal flow with current speed $U\left(z\right)$, the difference in the along-beam velocity $b$ observed between bin number $j$ and $j+n$ will be

7$$b(i,j)-b(i,j+n)=\sin \mathit{\theta }n\mathit{\delta }z{\displaystyle \frac{\partial U}{\partial z}},$$ where $\mathit{\theta }$ is the ADCP beam angle (from the instrument axis) and $\mathit{\delta }z$ is the vertical bin centre separation distance of the velocity measurement bins. Calculating the structure function with $b$ rather than $b^{\prime }$ fully retains these non-turbulent velocity differences such that 8$$D_{\mathrm{LL}}^{\mathrm{b}}(i,j,r_n)=r_n^{\mathrm{2}}{\sin }^{\mathrm{2}}\mathit{\theta }{\cos }^{\mathrm{2}}\mathit{\theta }{\left({\displaystyle \frac{\partial U}{\partial z}}\right)}^{\mathrm{2}}.$$ The standard method linear regression of $D_{\mathrm{LL}}^{\mathrm{b}}$ against $r^{\frac{\mathrm{2}}{\mathrm{3}}}$ as per Eq. () yields gradient $a_{\mathrm{1}}$, with Eq. () giving the potential bias TKE dissipation rate, ${\mathit{\epsilon }}^{\mathrm{b}}$.

Figure 2

Potential bias due to shear using the standard method regression when none of the non-turbulent velocity differences between bins due to shear are removed (${\mathit{\epsilon }}^{\mathrm{b}}$), evaluated for selected levels of shear $S^{\mathrm{2}}$, bin sizes $\mathit{\delta }z$, and maximum separation distance used for the regression $r_{\max }$.

[Figure omitted. See PDF]

Figure  illustrates the variation of ${\mathit{\epsilon }}^{\mathrm{b}}$ for an ADCP with a 20${}^{\circ }$ beam angle (standard for the Teledyne RDI WorkHorse), with the vertical bin size $\mathit{\delta }z$ varying between 0.1 and 0.5 m; the maximum separation distance used in the regression, $r_{\max }$, varying between 0.5 and 5 m subject to the minimum $r_{\max }=\mathrm{5}\mathit{\delta }r$; and shear-squared, $S^{\mathrm{2}}={\left(\frac{\partial U}{\partial z}\right)}^{\mathrm{2}}$, of $\mathrm{1}\times {\mathrm{10}}^{-\mathrm{5}}$ and $\mathrm{1}\times {\mathrm{10}}^{-\mathrm{4}}$ s${}^{-\mathrm{2}}$. For each permutation, ${\mathit{\epsilon }}^{\mathrm{b}}$ is calculated for a beam directly aligned with the sheared flow and for those bins for which all $r\le r_{\max }$ values are evaluated.

The bin sizes and $r_{\max }$ configurations evaluated are consistent with deployments in regions where mixing is of interest, such as the pycnocline in shelf seas, where shear levels frequently exceed $\mathrm{1}\times {\mathrm{10}}^{-\mathrm{4}}$ s${}^{-\mathrm{2}}$ and $\mathit{\epsilon }$ levels are commonly in the range $\mathrm{1}\times {\mathrm{10}}^{-\mathrm{9}}$ to $\mathrm{1}\times {\mathrm{10}}^{-\mathrm{7}}$ W kg${}^{-\mathrm{1}}$ e.g.. Figure  demonstrates that the potential bias ${\mathit{\epsilon }}^{\mathrm{b}}$, if wholly retained due to the motion of the ADCP, may be comparable to the $\mathit{\epsilon }$ levels being observed.

Figure  also illustrates that since $D_{\mathrm{LL}}^{\mathrm{b}}$ exhibits a linear dependence on $S^{\mathrm{2}}$, the regression coefficient $a_{\mathrm{1}}$ also varies linearly with $S^{\mathrm{2}}$; hence, ${\mathit{\epsilon }}^{\mathrm{b}}$ varies as $S^{\mathrm{3}}$. Consequently, increasing $S^{\mathrm{2}}$ from $\mathrm{1}\times {\mathrm{10}}^{-\mathrm{5}}$ to $\mathrm{1}\times {\mathrm{10}}^{-\mathrm{4}}$ m${}^{\mathrm{2}}$ s${}^{-\mathrm{2}}$ increases ${\mathit{\epsilon }}^{\mathrm{b}}$ by a factor of ${\mathrm{10}}^{\frac{\mathrm{3}}{\mathrm{2}}}$ for all $r_{\max }$ and $\mathit{\delta }z$ options.

The $r^{\mathrm{2}}$ length-scale dependency of $D_{\mathrm{LL}}^{\mathrm{b}}$ means that the standard method regression of Eq. () is imposing a least-squares linear fit against $r^{\frac{\mathrm{2}}{\mathrm{3}}}$ to a term varying as $(r^{\frac{\mathrm{2}}{\mathrm{3}}}{)}^{\mathrm{3}}$. The gradient $a_{\mathrm{1}}$ and hence ${\mathit{\epsilon }}^{\mathrm{b}}$ therefore increase rapidly with $r_{\max }$, whilst reducing the bin size increases the number of evaluated distances for a given $r_{\max }$, slightly reducing $a_{\mathrm{1}}$ and ${\mathit{\epsilon }}^{\mathrm{b}}$.

Whilst ${\mathit{\epsilon }}^{\mathrm{b}}$ can be derived for a known instrument configuration and anticipated shear, it is a theoretical maximum bias affecting beams directly aligned with the sheared flow and assuming all of the shear-related non-turbulent velocity difference between bins propagates through to the calculated structure function. The actual bias in the resolved $\mathit{\epsilon }$ values will be a fraction of ${\mathit{\epsilon }}^{\mathrm{b}}$ determined by the proportion of the non-turbulent velocity differences between bins due to the shear retained in $b^{\prime }$ as a consequence of the motion of the ADCP. Section  therefore uses long-term data on moored ADCPs configured for turbulence observations to examine how the motion of a tethered ADCP is influenced by the environmental conditions.

Quantifying the retained proportion of ${\mathit{\epsilon }}^{\mathrm{b}}$ under a wide range of ADCP motion scenarios when using the standard regression method, together with testing the effectiveness of the modified regression method based on Eq. () at reducing the bias, is then evaluated using synthesised velocity data in Sect. .

3 Field observations of ADCP motion

This section examines the heading and tilt sensor data from three inline tethered ADCPs deployed on a buoyancy-tensioned mooring at a site in the Celtic Sea with a water depth of 145 m over a 16-month period, providing data under a wide range of current and wave conditions. Details of the deployments and the data return together with information on the heading and tilt observations are given in Appendix .

Figure 3

Turbulence mooring diagram. Adapted from a figure in the RRS James Cook JC105 cruise report, which is available from the British Oceanographic Data Centre at http://www.bodc.ac.uk (last access: 19 January 2022).

[Figure omitted. See PDF]

3.1 Moorings

Three Teledyne RD Instruments (TRDI) 600 kHz WorkHorse ADCPs were deployed, with the nominal depths of the upper, middle, and lower instruments being 20, 33, and 50 m, respectively. The upper and lower instruments were deployed upwards-looking in spherical syntactic buoys, whilst the middle instrument was deployed downward-looking in an open frame as illustrated in Fig. . All had four-beam Janus-style transducer heads, with the upper and middle instruments having a 20${}^{\circ }$ beam angle and the lower a 30${}^{\circ }$ beam angle. The same configuration was used for all instruments and deployment periods, with a vertical bin size of 10 cm and the first bin centred 0.97 m vertically from the transducer head. Pulse–pulse coherent (TRDI mode 5) single-ping ensemble (no averaging) observations of along-beam velocity were made at 1 Hz for 5 min followed by 15 min sleep, yielding three bursts of observations per hour, each comprising 300 profiles for each beam. Velocities were typically resolved for bins 1 to 32 (1 to 29) for the 20${}^{\circ }$ (30${}^{\circ }$) beam angle instruments, consistent with the expected range for the operating mode .

Three-axis orientation data were recorded for each profile, providing a description of the instrument motion during each observation burst. As illustrated in Fig. , heading, ${\mathit{\varphi }}_{\mathrm{H}}$ (${}^{\circ }$ N), is the rotation about the vertical axis expressed as the compass direction of the horizontal projection of beam 3, whilst tilt sensors describe the rotation about the horizontal axes, with pitch, ${\mathit{\varphi }}_{\mathrm{P}}$ (${}^{\circ }$), being rotation in the plane of beams 3 and 4, roll, ${\mathit{\varphi }}_{\mathrm{R}}$ (${}^{\circ }$), being rotation in the plane of beams 1 and 2, and both ${\mathit{\varphi }}_{\mathrm{P}}$ and ${\mathit{\varphi }}_{\mathrm{R}}$ being zero, indicating that the instrument is vertical .

The along-beam velocity data for each profile were converted to Earth coordinates following . The burst mean horizontal velocities were depth-averaged over the $\sim \mathrm{3}$ m range of the observations and the dominant tidal constituents identified using the U-Tide MATLAB functions . The site is characterised by clockwise rotating semi-diurnal tides, with a pronounced spring–neap variation. Over the full deployment period, the horizontal current speed, $U$, observed by the upper instrument had a median value of 0.28 m s${}^{-\mathrm{1}}$, with $U\le \mathrm{0.1}$ m s${}^{-\mathrm{1}}$ for just 4.1 % of observations, with the implication being that the ADCP mooring was under almost continual drag, rotating semi-diurnally about the position of the anchor weight.

A UK Met Office Ocean Data Acquisition System (ODAS) buoy and a Triaxys frequency-direction wave buoy were moored less than 1 km away, providing hourly meteorological data, wave statistics, and spectra. Significant wave height was derived from the wave spectra data as

9$$H_{m_{\mathrm{0}}}=\mathrm{4}\sqrt{\sum _{n=\mathrm{1}}^{\mathrm{32}}{S}_f\left(n\right)\mathit{\delta }f\left(n\right)},$$ where $n$ is the wave frequency band number, $S_f\left(n\right)$ is the surface displacement variance (or “wave energy density”) per unit frequency (m${}^{\mathrm{2}}$ Hz${}^{-\mathrm{1}}$) for band $n$, and $\mathit{\delta }f\left(n\right)$ is the width of the frequency band (Hz). The $\mathrm{32}$ frequency bands of the Triaxys buoy have central frequencies between 0.03 and 0.6 Hz with widths increasing from 0.005 to 0.08 Hz.

The annual median $H_{m_{\mathrm{0}}}$ was 2.54 m, with 90 % of observations $\ge \mathrm{1.25}$ m and 10 % $\ge \mathrm{5.03}$ m. There was a significant seasonal variation, with over 90 % of observations during the “summer” deployment 2 (19 June to 21 August 2014) being less than the annual median and almost 23 % of observations during the “winter” deployment 4 (21 November 2014 to 4 April 2015) exceeding the annual 90th percentile.

Figure 4

Sample heading data. Panel (a) shows the Earth coordinate current speed $U$ (solid lines) and direction (to), $\mathrm{\Phi }$, (markers), and panel (b) shows the heading, ${\mathit{\varphi }}_{\mathrm{H}}$, for each ADCP (colour). Panels (c) to (e) show the variation in ${\mathit{\varphi }}_{\mathrm{H}}$, pitch (${\mathit{\varphi }}_{\mathrm{P}}$), and roll (${\mathit{\varphi }}_{\mathrm{R}}$), respectively, for the bursts indicated by the green box in panel (b).

[Figure omitted. See PDF]

3.2 ADCP motion sample

Panels (a) and (b) of Fig.  show sample data for a 30 h period, with the solid lines in panel (a) showing the depth-averaged burst mean horizontal current speed, $U$, the markers showing the compass direction (to), $\mathrm{\Phi }$, from the Earth coordinate velocity calculated for each burst profile, and the colour indicating the instrument. Panel (b) shows the ${\mathit{\varphi }}_{\mathrm{H}}$ data for each instrument for all bursts over the same period.

All three instruments are in close agreement for $U$, which varies over the range 0.2 to 0.5 m s${}^{-\mathrm{1}}$. Current direction, $\mathrm{\Phi }$, shows the tide rotating clockwise, with the $U$ maxima coinciding with the flow being towards the south-west and the north-east. For the upper and lower instruments, $\mathrm{\Phi }$, is in good agreement throughout the period. For the middle instrument, there are differences of up to $\pm \mathrm{30}$${}^{\circ }$, reflecting anomalies in the instrument heading data apparent in panel (b). Prior to circa 02:00 on 7 February 2015, $\mathrm{\Phi }$ is in close agreement with the other instruments. The burst mean heading, $⟨{\mathit{\varphi }}_{\mathrm{H}}⟩$, exhibits a steady clockwise rotation, is then reduced by $\sim \mathrm{60}$${}^{\circ }$ between bursts, and remains fairly constant over a 2 h period (7 bursts), at the end of which it jumps by $\sim \mathrm{90}$${}^{\circ }$ and reverts to tracking the rotating tide. During this hiatus, both $U$ and $\mathrm{\Phi }$ are in excellent agreement with the other instruments, but the subsequent jump in $⟨{\mathit{\varphi }}_{\mathrm{H}}⟩$ introduces an offset of $\sim -\mathrm{30}$${}^{\circ }$ in $\mathrm{\Phi }$. Approximately 4 h later, the offset changes sign over a period of $\sim \mathrm{1}$ h, the transition coinciding with $⟨{\mathit{\varphi }}_{\mathrm{H}}⟩$ progressing through 360/0${}^{\circ }$. The offset subsequently changes sign again as $⟨{\mathit{\varphi }}_{\mathrm{H}}⟩$ increases past 180${}^{\circ }$ and again when it next progresses through 360/0${}^{\circ }$. A second sudden change in $⟨{\mathit{\varphi }}_{\mathrm{H}}⟩$ between bursts occurs at circa 20:00 the same day, just prior to the second transition through 360/0${}^{\circ }$, but affects just a single burst.

The incidence of such events was rare, with no clear periodicity apparent, albeit mostly occurring when $U$ was low during neap tides, suggesting the possibility of a mechanical cause. However, the coincidence of the change in sign of the offset in $\mathrm{\Phi }$ with the progression of $⟨{\mathit{\varphi }}_{\mathrm{H}}⟩$ through 180 and 360/0${}^{\circ }$ suggests the possibility of a compass sensor problem. Despite this issue affecting the calculation of the Earth coordinate current direction for some bursts, there is no indication of any problems with the variation of ${\mathit{\varphi }}_{\mathrm{H}}$ during a burst.

Panel (b) shows that the variation in ${\mathit{\varphi }}_{\mathrm{H}}$ was limited during the majority of bursts. However, in each of two successive bursts at circa 20:00 on 7 February, the lower instrument completes an anticlockwise rotation over a period of $\sim \mathrm{90}$ s, with the heading then returning to a value similar to that prior to the rotation. Over the rest of the burst, the heading varies over a range $\sim \mathrm{30}$${}^{\circ }$ as in other bursts. The events coincide with $U$ being at a minimum, and the direction of rotation is opposite to the rotation of the tide, suggesting the effect may be due to a relaxation of accumulated tension in the mooring.

Panels (c) to (e) show the time series of ${\mathit{\varphi }}_{\mathrm{H}}$, ${\mathit{\varphi }}_{\mathrm{P}}$, and ${\mathit{\varphi }}_{\mathrm{R}}$ for the individual burst identified by the green box in panel (b). The plots show that the instruments all oscillate throughout the period of the burst, with the frequency and amplitude of the oscillation varying between instruments. The range and frequency of these oscillations are examined further in the following sections and in Appendix .

3.3 Heading variation

For each ADCP and deployment period, the instrument heading, ${\mathit{\varphi }}_{\mathrm{H}}$, typically oscillated around a burst mean that rotated with the tide. For each burst, the heading data were analysed as the burst maximum heading range, $\mathrm{\Delta }{\mathit{\varphi }}_{\mathrm{H}}$, evaluated as the absolute difference between the minimum and maximum ${\mathit{\varphi }}_{\mathrm{H}}$ expressed on a continuous basis such that if the instrument completes a full rotation during the burst, $\mathrm{\Delta }{\mathit{\varphi }}_{\mathrm{H}}\ge \mathrm{360}$${}^{\circ }$, and the number of heading oscillations per burst, $n_{{\mathit{\varphi }}_{\mathrm{H}}}$, evaluated as the number of times ${\mathit{\varphi }}_{\mathrm{H}}$ increased above the burst mean heading, $⟨{\mathit{\varphi }}_{\mathrm{H}}⟩$, such that ${\mathit{\varphi }}_{\mathrm{H}}-⟨{\mathit{\varphi }}_{\mathrm{H}}⟩$ changed from negative to positive.

Statistics for each instrument and deployment period are included in Appendix . The middle instrument, mounted in an open frame, exhibited the largest-amplitude oscillations, with $\mathrm{\Delta }{\mathit{\varphi }}_{\mathrm{H}}\ge \mathrm{180}$${}^{\circ }$ in more than 9 % of bursts during the “autumn” deployment period 3 (22 August to 20 November 2014) and approximately 7 % of bursts during the winter deployment period 4 compared with 1 % to 2 % for the upper and lower instruments. The middle instrument was also typically subject to more oscillations per burst than the other instruments. The lower instrument typically exhibited the fewest and smallest-amplitude oscillations.

Figure 5

Mean heading oscillation range $\stackrel{\mathrm{‾}}{\mathrm{\Delta }{\mathit{\varphi }}_{\mathrm{H}}}$ (${}^{\circ }$) (a–c), mean heading oscillations per burst $\stackrel{\mathrm{‾}}{n_{{\mathit{\varphi }}_{\mathrm{H}}}}$ (d–f), and percentage of bursts (g–i) for bursts aggregated by current speed, $U$ (m s${}^{-\mathrm{1}}$), and significant wave height, $H_{m_{\mathrm{0}}}$ (m), for the deployment period 22 November 2014 to 4 April 2015, with aggregation bin $\mathit{\delta }U=\mathrm{0.0175}$ m s${}^{-\mathrm{1}}$ and $\mathit{\delta }{H}_{m_{\mathrm{0}}}=\mathrm{0.3}$ m. The instrument mooring position is shown above each column.

[Figure omitted. See PDF]

Figure  illustrates the variation of $\mathrm{\Delta }{\mathit{\varphi }}_{\mathrm{H}}$ and $n_{{\mathit{\varphi }}_{\mathrm{H}}}$ with the concurrent tidal current speed, $U$, and spectral significant wave height, $H_{m_{\mathrm{0}}}$, for the winter deployment period 4. $U$ is the current speed from the burst mean horizontal Earth coordinate velocity components, depth-averaged across the reliably resolved bin levels. $H_{m_{\mathrm{0}}}$ is calculated from the Triaxys buoy data as per Eq. () and interpolated to the ADCP observation times. Bursts are aggregated based on $U$ and $H_{m_{\mathrm{0}}}$ for $\mathrm{0}\mathrm{m}{\mathrm{s}}^{-\mathrm{1}}\le U\le \mathrm{0.7}\mathrm{m}{\mathrm{s}}^{-\mathrm{1}}$ and $\mathrm{0}\mathrm{m}\le H_{m_{\mathrm{0}}}\le \mathrm{12}\mathrm{m}$ with aggregation bin sizes $\mathit{\delta }U=\mathrm{0.0175}$ m s${}^{-\mathrm{1}}$ and $\mathit{\delta }{H}_{m_{\mathrm{0}}}=\mathrm{0.3}$ m. The left, centre, and right columns show the data for the upper, middle, and lower ADCP, respectively.

Panels (a) to (c) show the mean of the maximum heading range, $\stackrel{\mathrm{‾}}{\mathrm{\Delta }{\mathit{\varphi }}_{\mathrm{H}}}$, for the bursts in each $(\mathit{\delta }U,\mathit{\delta }{H}_{m_{\mathrm{0}}})$ aggregation bin; panels (d) to (f) the mean number of heading oscillations, $\stackrel{\mathrm{‾}}{n_{{\mathit{\varphi }}_{\mathrm{H}}}}$; and panels (g) to (i) the percentage of bursts in each bin. Plots for the other deployment periods (not shown) demonstrate the same basic patterns, subject to the more limited $H_{m_{\mathrm{0}}}$ range.

For all instruments, $\stackrel{\mathrm{‾}}{\mathrm{\Delta }{\mathit{\varphi }}_{\mathrm{H}}}$ is highest when $U$ is low, tending to decrease with increasing $U$. There is also evidence of $\stackrel{\mathrm{‾}}{\mathrm{\Delta }{\mathit{\varphi }}_{\mathrm{H}}}$ increasing with $H_{m_{\mathrm{0}}}$, most clearly for the middle instrument. Conversely, $\stackrel{\mathrm{‾}}{n_{{\mathit{\varphi }}_{\mathrm{H}}}}$, exhibits a clear tendency to increase with $U$ for all instruments but is relatively insensitive to variations in $H_{m_{\mathrm{0}}}$. The rate at which $\stackrel{\mathrm{‾}}{n_{{\mathit{\varphi }}_{\mathrm{H}}}}$ increases with $U$ varies between the instruments, but they all exhibit the same basic response.

The variation from a few large oscillations at low $U$ to an increasing number of smaller-amplitude oscillations at higher $U$ is consistent with the oscillations being primarily a hydraulic response. The relatively higher values of $\stackrel{\mathrm{‾}}{\mathrm{\Delta }{\mathit{\varphi }}_{\mathrm{H}}}$ and $\stackrel{\mathrm{‾}}{n_{{\mathit{\varphi }}_{\mathrm{H}}}}$ for the middle instrument suggest that the open frame housing is more susceptible to motion than the spherical housing used for the other instruments.

Figure 6

Mean tilt $\stackrel{\mathrm{‾}}{\mathit{\delta }⟨\mathit{\alpha }⟩}$ (${}^{\circ }$) (a–c), mean tilt range $\stackrel{\mathrm{‾}}{\mathrm{\Delta }\mathit{\alpha }}$ (${}^{\circ }$) (d–f), and mean tilt oscillations per burst $\stackrel{\mathrm{‾}}{n_{{\mathit{\varphi }}_{\mathrm{H}}}}$ (g–i) for bursts aggregated by current speed, $U$ (m s${}^{-\mathrm{1}}$), and significant wave height, $H_{m_{\mathrm{0}}}$ (m), for the deployment period 22 November 2014 to 4 April 2015, with aggregation bin $\mathit{\delta }U=\mathrm{0.0175}$ m s${}^{-\mathrm{1}}$ and $\mathit{\delta }{H}_{m_{\mathrm{0}}}=\mathrm{0.3}$ m. The instrument mooring position is shown above each column.

[Figure omitted. See PDF]

3.4 Tilt variation

The pitch and roll data for each profile were used to compute the tilted beam angle relative to the vertical, ${\mathit{\alpha }}_i$ (${}^{\circ }$), for each beam $i$, as described in Appendix . Figure  illustrates the dependence of beam tilt on concurrent $U$ and $H_{m_{\mathrm{0}}}$ during the winter deployment period 4. Mean values are again taken across bursts aggregated in $(\mathit{\delta }U$, $\mathit{\delta }{H}_{m_{\mathrm{0}}})$ bins, where $\mathit{\delta }U$ is 0.0175 m s${}^{-\mathrm{1}}$ and $\mathit{\delta }{H}_{m_{\mathrm{0}}}$ is 0.3 m. Data for the upper, middle, and lower instruments are shown in the left, centre, and right columns, respectively.

Panels (a) to (c) show the mean absolute burst tilt across all beams, $\stackrel{\mathrm{‾}}{\mathit{\delta }⟨\mathit{\alpha }⟩}$, where $\mathit{\delta }⟨\mathit{\alpha }⟩=\underset{\mathrm{¯}}{|⟨{\mathit{\alpha }}_i⟩-\mathit{\theta }|}$, with $⟨{\mathit{\alpha }}_i⟩$ being the burst mean tilt for beam $i$, the vertical bars indicating the absolute value, and the underline indicating the mean across the beams. Panels (d) to (f) show the mean of the beam tilt variation range, $\stackrel{\mathrm{‾}}{\mathrm{\Delta }\mathit{\alpha }}$, with $\mathrm{\Delta }\mathit{\alpha }$ being the mean across the beams of the difference between the burst maximum and minimum ${\mathit{\alpha }}_i$ values for beam $i$. Panels (g) to (i) show the mean beam tilt oscillations per burst, $\stackrel{\mathrm{‾}}{n_{\mathit{\alpha }}}$, where $n_{\mathit{\alpha }}$ is the mean across the beams of $n_{{\mathit{\alpha }}_i}$, which is evaluated as the number of times the sign of ${\mathit{\alpha }}_i-⟨{\mathit{\alpha }}_i⟩$ changes from negative to positive during the burst. The plots for other deployment periods (not shown) are similar, subject to the more limited $H_{m_{\mathrm{0}}}$ range.

The mean beam tilt angle, $\stackrel{\mathrm{‾}}{\mathit{\delta }⟨\mathit{\alpha }⟩}$, exhibits a clear dependence on $U$, increasing with increasing $U$ for all instruments, with the effect being relatively weaker for the upper instrument and strengthening with instrument depth. The mean beam tilt angle inevitably understates the tilt for individual beams, e.g. for the lower instrument $\stackrel{\mathrm{‾}}{\mathit{\delta }⟨\mathit{\alpha }⟩}\ge \mathrm{10}$${}^{\circ }$ for just 0.6 % of bursts during deployment 4, although 4.6 % of bursts had at least one beam with that level of tilt. In such circumstances the opposing beams will differ significantly in their orientation to the prevailing current, as well as spanning different vertical ranges.

The mean burst tilt range, $\stackrel{\mathrm{‾}}{\mathrm{\Delta }\mathit{\alpha }}$, clearly increases with increasing $H_{m_{\mathrm{0}}}$, suggesting that the range of the rocking motion about the tilt axes is primarily driven by the surface-wave-forced orbital motion. This is consistent with the upper buoy on the mooring rising and falling with the wave, thereby varying the vertical angle of the mooring. Some tendency for $\stackrel{\mathrm{‾}}{\mathrm{\Delta }\mathit{\alpha }}$ to increase with increasing $U$ is also apparent for the middle instrument and, to a lesser extent, the upper instrument. Large ranges are observed for both the upper and middle instrument, with the mean across the beams exceeding 20${}^{\circ }$ in 0.3 % of bursts and at least one beam exceeding 20${}^{\circ }$ in 1.3 % of bursts for the middle instrument during this deployment period; the equivalent figures for the upper instrument are 0.2 % and 1.0 %, respectively. The beam tilt range is significantly reduced for the lower instrument, consistent with $\mathrm{\Delta }\mathit{\alpha }$ being influenced by surface waves.

The variation in the mean beam tilt oscillation frequency, as indicated by $\stackrel{\mathrm{‾}}{n_{\mathit{\alpha }}}$, is relatively limited. The highest values affect the middle and lower instruments and occur at low $H_{m_{\mathrm{0}}}$ but with no consistent trends.

4 Retained bias in synthesised sheared flow

The observations demonstrate that tethered ADCPs may be subject to both a mean tilt due to drag on the mooring and significant oscillatory variation in both heading and tilt over the period of an observation burst. In the presence of a sheared flow, this motion will unavoidably result in a proportion of the non-turbulent velocity difference between bins being retained in $b^{\prime }$, contributing to the structure function and biassing the $\mathit{\epsilon }$ estimates derived using the standard regression method.

This retained bias was investigated using synthesised velocities for a range of scenarios with the ADCP subject to oscillatory variations in heading, pitch, and roll. For each scenario, along-beam velocities, $b$, were synthesised for a burst of observations following the procedure detailed in Appendix . The ADCP geometry was based on the TRDI WorkHorse ADCP, with a default beam angle $\mathit{\theta }=\mathrm{20}$${}^{\circ }$ and a vertical bin size $\mathit{\delta }z=\mathrm{0.1}$ m, with bin 1 centred at $\mathit{\delta }{z}_{\mathrm{1}}=\mathrm{1}$ m and 30 bins per beam. The default observation burst comprised 300 profiles at 1 Hz.

The residual velocity, $b^{\prime }$, was calculated by deducting the burst mean, $b^{\prime }=b-⟨b⟩$, and the second-order longitudinal structure function, $D_{\mathrm{LL}}(i,j,r_n)$, evaluated as per Eq. () using a bin-centred difference scheme for each beam $i$, bin $j$, and all possible bin separation distances, $r_n$, based on multiples of the along-beam bin size $\mathit{\delta }r=\mathit{\delta }z/\cos \mathit{\theta }$ . TKE dissipation rate values, ${\mathit{\epsilon }}^s$, were calculated using the standard regression method of a least-squares linear regression to Eq. () with $r_{\max }=\mathrm{2.02}$ m (equivalent to a maximum separation of 19 bins) and including the single bin separation and the Eq. () constant $C_{\mathrm{2}}=\mathrm{2.0}$, with the superscript indicating that the values are from synthesised data. The depth-average ${\mathit{\epsilon }}_i^s$ for beam $i$ was taken as the mean across bins 11 to 20 for which all $r_n\le r_{\max }$ values were evaluated.

No turbulence was introduced in the along-beam velocities or the structure function; therefore, ${\mathit{\epsilon }}_i^s$ was the retained bias due to the motion of the ADCP.

${\mathit{\epsilon }}_i^s$ values were normalised as a proportion of the potential bias, ${\mathit{\epsilon }}_{\mathrm{45}}^{\mathrm{b}}$, calculated from the along-beam velocity, $b$, for the same background flow and ADCP configuration, with the ADCP vertical, static, and oriented with the heading at 45${}^{\circ }$ to the background flow direction such that each beam has the same difference angle to the flow and therefore the same potential bias.

The default background flow was specified with a speed at the ADCP transducer head $U_{\mathrm{0}}=\mathrm{0.25}$ m s${}^{-\mathrm{1}}$, with depth constant direction (to) $\mathit{\beta }=\mathrm{90}$${}^{\circ }$ N, shear $S^{\mathrm{2}}=\mathrm{1}\times {\mathrm{10}}^{-\mathrm{4}}$ s${}^{-\mathrm{2}}$, and no surface waves. Testing confirmed that the results were insensitive to $U_{\mathrm{0}}$ and that both ${\mathit{\epsilon }}_i^s$ and ${\mathit{\epsilon }}_{\mathrm{45}}^{\mathrm{b}}$ scaled as $S^{\mathrm{3}}$ such that ${\mathit{\epsilon }}_i^s/{\mathit{\epsilon }}_{\mathrm{45}}^{\mathrm{b}}$ was independent of $S^{\mathrm{2}}$.

Figure 7

Illustration of heading oscillation in a sheared current, with ${\mathit{\varphi }}_{\mathrm{H}}\left(\mathrm{0}\right)=\mathrm{90}$${}^{\circ }$ N, $\mathrm{\Delta }{\mathit{\varphi }}_{\mathrm{H}}=\mathrm{60}$${}^{\circ }$, $t_{{\mathit{\varphi }}_{\mathrm{H}}}=\mathrm{30}$ s, and ${\mathit{\varphi }}_{\mathrm{P}}\left(t\right)$ and ${\mathit{\varphi }}_{\mathrm{R}}\left(t\right)$ both 0${}^{\circ }$ for all $t$. Panel (a) shows the beam sweep with lines indicating the positions of bins $\mathrm{1},\mathrm{5},\mathrm{10},\mathrm{15}\mathrm{\dots }\mathrm{30}$; markers indicate bin 30 centre position at times $t=\mathrm{0}$ s (circle), 2 s (square), 8 s (diamond), and 22 s (triangle), and grey arrows indicate the sheared mean current (not to scale). Panels (b) to (d) show the first 30 s of the 300 s duration burst time series for bin 16 of each beam (colours as per panel a legend) for (b) the along-beam velocity $b$ (m s${}^{-\mathrm{1}}$), (c) the bin-centred difference of the residual velocity $\mathit{\delta }{b}_i^{\prime }$ (mm s${}^{-\mathrm{1}}$) for $r$ of $\mathrm{19}\mathit{\delta }r$, and (d) the squared velocity difference $[\mathit{\delta }{b}_i^{\prime }{]}^{\mathrm{2}}$ (mm${}^{\mathrm{2}}$ s${}^{-\mathrm{2}}$), with the grey markers in each panel indicating the times of the corresponding shape bin 30 position markers in panel (a). Panel (e) shows the second-order structure function, $D_{\mathrm{LL}}$ (m${}^{\mathrm{2}}$ s${}^{-\mathrm{2}}$), for beams 1 (blue line), 2 (red bullet), 3 (yellow line), and 4 (purple bullet), with $r_{\max }$ indicated by the vertical green line, as well as the linear regressions for beams 1 and 3 (dotted lines), with the annotation showing the normalised residual bias ${\mathit{\epsilon }}_i^s/{\mathit{\epsilon }}_{\mathrm{45}}^{\mathrm{b}}$ for each beam.

[Figure omitted. See PDF]

4.1 Heading variation example

Figure  illustrates the impact of heading oscillation for an example scenario. Initial heading ${\mathit{\varphi }}_{\mathrm{H}}\left(\mathrm{0}\right)$ and mean current direction $\mathit{\beta }$ are both 90${}^{\circ }$ N. The heading oscillation range is $\mathrm{\Delta }{\mathit{\varphi }}_{\mathrm{H}}=\mathrm{60}$${}^{\circ }$ and the period $t_{{\mathit{\varphi }}_{\mathrm{H}}}=\mathrm{30}$ s, and the instrument is vertical, with ${\mathit{\varphi }}_{\mathrm{P}}\left(t\right)$ and ${\mathit{\varphi }}_{\mathrm{R}}\left(t\right)$ zero for all $t$.

Panel (a) shows the variation in the synthesised ADCP bin positions in an $[x,y,z]$ coordinate framework referenced to the transducer head; see Appendix . The sweep of each of the beams is shown by the shaded areas, with lines indicating the positions for bins $\mathrm{1},\mathrm{5},\mathrm{10},\mathrm{15}\mathrm{\dots }\mathrm{30}$ and markers for the bin 30 centre position at times $t=\mathrm{0}$ s (circle), 2 s (square), 8 s (diamond), and 22 s (triangle).

The first 30 s of the synthesised along-beam velocity time series for bin 16 in each beam $i$, $b_i(\mathrm{16},t)$ (m s${}^{-\mathrm{1}}$), is shown in panel (b), with the variation repeating over the 300 s duration of the burst. Beam 1 (blue line) is initially oriented across the background flow such that $b_{\mathrm{1}}(\mathrm{16},\mathrm{0})$ is zero ($t=\mathrm{0}$ s, circle marker). As the heading changes, beam 1 initially points increasingly upstream (square marker at $t=\mathrm{2}$ s) and $b_{\mathrm{1}}(\mathrm{16},t)$ varies with the sine of the heading difference angle, reaching a positive maximum at $t_{{\mathit{\varphi }}_{\mathrm{H}}}/\mathrm{4}$ when ${\mathit{\varphi }}_{\mathrm{H}}\left(t\right)={\mathit{\varphi }}_{\mathrm{H}}\left(\mathrm{0}\right)+\mathrm{\Delta }{\mathit{\varphi }}_{\mathrm{H}}/\mathrm{2}$ (just before the diamond marker at $t=\mathrm{8}$ s). The heading then rotates back towards the mean position and $b_{\mathrm{1}}(\mathrm{16},t)$ is reduced to zero at $t_{{\mathit{\varphi }}_{\mathrm{H}}}/\mathrm{2}$. As the oscillation continues, $b_{\mathrm{1}}(\mathrm{16},t)$ reaches a maximum negative at $\mathrm{3}{t}_{{\mathit{\varphi }}_{\mathrm{H}}}/\mathrm{4}$ (close to the triangle marker at $t=\mathrm{22}$ s) and returns to zero at $t_{{\mathit{\varphi }}_{\mathrm{H}}}$, with the oscillation repeating until the end of the burst. Since the ADCP is vertical, symmetry means that $b_{\mathrm{2}}(\mathrm{16},t)$ (red line) has the same magnitude but opposite sign as $b_{\mathrm{1}}(\mathrm{16},t)$ for all $t$.

Beam 3 (yellow line) is initially oriented directly downstream so that $b_{\mathrm{3}}(\mathrm{16},\mathrm{0})$ has a maximum negative value. As the heading changes, the magnitude of $b_{\mathrm{3}}(\mathrm{16},t)$ is reduced as the cosine of the heading difference angle, reaching a minimum at $t_{{\mathit{\varphi }}_{\mathrm{H}}}/\mathrm{4}$ and then increasing to regain its maximum value at $t_{{\mathit{\varphi }}_{\mathrm{H}}}/\mathrm{2}$, with the variation repeating over the second half of the oscillation period. Compared with $b_{\mathrm{1}}(\mathrm{16},t)$, $b_{\mathrm{3}}(\mathrm{16},t)$ varies with double the oscillation frequency but a much smaller amplitude and has a non-zero mean. Symmetry again means that the $b_{\mathrm{4}}(\mathrm{16},t)$ (purple line) has the same magnitude as $b_{\mathrm{3}}(\mathrm{16},t)$ but opposite sign.

Since the burst mean for beams 1 and 2 is approximately zero, the periodic variation in $b$ is fully retained in $b^{\prime }$, including any velocity differences between bins due to the sheared flow. Conversely, for beams 3 and 4, the variation in $b$ is greatly reduced so that the majority of velocity difference between bins is not retained in $b^{\prime }$. This is reflected in panel (c), which shows the time series for $\mathit{\delta }{b}^{\prime }$ for bin 16 with $r_n=r_{\max }$ ($\mathrm{19}\mathit{\delta }r$) for each beam, $\mathit{\delta }{b}_i^{\prime }(\mathrm{16},\mathrm{19}\mathit{\delta }r)$ (mm s${}^{-\mathrm{1}}$). The opposing beams in each beam pair have identical values but opposite sign, whilst the magnitude of the oscillation for beams 1 and 2 is clearly much larger than that for beams 3 and 4.

Panel (d) shows the time series for the squared velocity difference ${\left[\mathit{\delta }{b}_i^{\prime }(\mathrm{16},\mathrm{19}\mathit{\delta }r)\right]}^{\mathrm{2}}$ (mm${}^{\mathrm{2}}$ s${}^{-\mathrm{2}}$), which is positive for all $t$. Values for the opposing beam pairs are identical, with the burst mean for beams 1 and 2 (red line overlying blue line) clearly significantly larger than that for beams 3 and 4 (purple line overlying yellow line).

Panel (e) shows the structure function $D_{\mathrm{LL}}(i,\mathrm{16})$ for each beam and a range of $r_n$ values, including $r_{\max }$ indicated by the vertical green line, plotted against $r^{\frac{\mathrm{2}}{\mathrm{3}}}$, demonstrating both the marked difference between the beam pairs and the non-linear growth of $D_{\mathrm{LL}}$ with $r^{\frac{\mathrm{2}}{\mathrm{3}}}$. Again, beams 1 (solid blue line) and 2 (red bullet markers) are identical, as are beams 3 (solid yellow line) and 4 (purple bullet markers). The dotted blue (beam 1) and yellow (beam 3) lines indicate the linear regression fit for all $r_n\le r_{\max }$ with no restriction on the regression intercept.

The annotation in panel (e) shows the normalised residual bias ${\mathit{\epsilon }}_i^s/{\mathit{\epsilon }}_{\mathrm{45}}^{\mathrm{b}}$ for each beam, indicating the retained fraction of the potential bias in each beam. For this scenario the residual bias arises almost exclusively in beams 1 and 2, which have a mean alignment across the current direction and are only exposed to the current by the oscillation, whilst the contribution from beams 3 and 4, which are closely aligned with the current direction, is negligible.

4.2 Heading variation scenarios

The potential impact of the heading varying was evaluated across scenarios with ${\mathit{\varphi }}_{\mathrm{H}}\left(\mathrm{0}\right)$ varied in 5${}^{\circ }$ increments over the range 30 to 150${}^{\circ }$ N, $\mathrm{\Delta }{\mathit{\varphi }}_{\mathrm{H}}$ varied in 10${}^{\circ }$ increments over the range 0 to 450${}^{\circ }$, and 18 $t_{{\mathit{\varphi }}_{\mathrm{H}}}$ options over the range 10 to 360 s with the ADCP vertical for all scenarios, i.e. ${\mathit{\varphi }}_{\mathrm{P}}\left(t\right)$ and ${\mathit{\varphi }}_{\mathrm{R}}\left(t\right)$ being 0${}^{\circ }$ for all $t$, yielding 20 275 scenarios. The ranges for $\mathrm{\Delta }{\mathit{\varphi }}_{\mathrm{H}}$ and $t_{{\mathit{\varphi }}_{\mathrm{H}}}$ were chosen taking account of the variation in the observations described in Sect.  and with the aim of encompassing the likely range of impacts.

Figure 8

Normalised residual bias for heading oscillation scenarios. (a) Variation of beam-averaged normalised residual bias, ${\underset{\mathrm{¯}}{\mathit{\epsilon }}}^s/{\mathit{\epsilon }}_{\mathrm{45}}^{\mathrm{b}}$, with initial heading offset angle to the background flow, $\mathit{\psi }$, for selected heading oscillation ranges $\mathrm{\Delta }{\mathit{\varphi }}_{\mathrm{H}}$ and fixed heading oscillation period $t_{{\mathit{\varphi }}_{\mathrm{H}}}=\mathrm{30}$ s. (a) Mean ${\underset{\mathrm{¯}}{\mathit{\epsilon }}}^s/{\mathit{\epsilon }}_{\mathrm{45}}^{\mathrm{b}}$ (black line), with 25 % to 75 % range (dark grey shading) and 5 % to 95 % range (light grey shading) for scenarios aggregated by $\mathrm{\Delta }{\mathit{\varphi }}_{\mathrm{H}}$. (c) Mean and ranges for the maximum normalised beam residual bias ${\mathit{\epsilon }}_i^s/{\mathit{\epsilon }}_{\mathrm{45}}^{\mathrm{b}}$ as in panel (b). The vertical lines in panels (b) and (c) are the deployment 4 median (dotted line) and 90th percentile (solid line) $\mathrm{\Delta }{\mathit{\varphi }}_{\mathrm{H}}$ values for the upper (grey) and middle (black) instruments from the observations described in Sect. .

[Figure omitted. See PDF]

The results are summarised in Fig. . Panel (a) shows the variation of the beam-averaged normalised residual bias, ${\underset{\mathrm{¯}}{\mathit{\epsilon }}}^s/{\mathit{\epsilon }}_{\mathrm{45}}^{\mathrm{b}}$, with the underline indicating the mean of ${\mathit{\epsilon }}_i^s$ across the four beams, the difference angle between the initial ADCP heading and the background flow direction, $\mathit{\psi }=\mathit{\beta }-{\mathit{\varphi }}_{\mathrm{H}}\left(\mathrm{0}\right)$, for selected heading oscillation ranges, $\mathrm{\Delta }{\mathit{\varphi }}_{\mathrm{H}}$, and a fixed heading oscillation period $t_{{\mathit{\varphi }}_{\mathrm{H}}}$ of 30 s. Since the heading oscillates around ${\mathit{\varphi }}_{\mathrm{H}}\left(\mathrm{0}\right)$, the burst mean heading is $⟨{\mathit{\varphi }}_{\mathrm{H}}⟩\approx {\mathit{\varphi }}_{\mathrm{H}}\left(\mathrm{0}\right)$, with any slight difference arising from the burst period not being an exact multiple of the oscillation period. Hence, $\mathit{\psi }$ is also the burst mean heading offset angle relative to the background flow.

For each $\mathrm{\Delta }{\mathit{\varphi }}_{\mathrm{H}}$, there is a limited variation in ${\underset{\mathrm{¯}}{\mathit{\epsilon }}}^s/{\mathit{\epsilon }}_{\mathrm{45}}^{\mathrm{b}}$ with $\mathit{\psi }$, which is highest when $\mathit{\psi }=\mathrm{0}$${}^{\circ }$ and lowest for $\mathit{\psi }=\pm \mathrm{45}$${}^{\circ }$, with the ratio between the minimum and the maximum decreasing with increasing $\mathrm{\Delta }{\mathit{\varphi }}_{\mathrm{H}}$. This variation is superimposed on the clear trend for ${\underset{\mathrm{¯}}{\mathit{\epsilon }}}^s/{\mathit{\epsilon }}_{\mathrm{45}}^{\mathrm{b}}$ to increase with $\mathrm{\Delta }{\mathit{\varphi }}_{\mathrm{H}}$, as indicated by comparing the lines for the selected options. This is illustrated further in panel (b), which shows the mean ${\underset{\mathrm{¯}}{\mathit{\epsilon }}}^s/{\mathit{\epsilon }}_{\mathrm{45}}^{\mathrm{b}}$ (black line), together with the 25 % to 75 % (dark grey shading) and 5 % to 95 % (light grey shading) ranges for scenarios aggregated on the basis of $\mathrm{\Delta }{\mathit{\varphi }}_{\mathrm{H}}$, combining scenarios with the various $\mathit{\psi }$ and $t_{{\mathit{\varphi }}_{\mathrm{H}}}$ options. Mean ${\underset{\mathrm{¯}}{\mathit{\epsilon }}}^s/{\mathit{\epsilon }}_{\mathrm{45}}^{\mathrm{b}}$ is negligible for $\mathrm{\Delta }{\mathit{\varphi }}_{\mathrm{H}}\le \mathrm{50}$${}^{\circ }$, then increases to reach a maximum of $\sim \mathrm{1}$ at $\mathrm{\Delta }{\mathit{\varphi }}_{\mathrm{H}}\sim \mathrm{270}$${}^{\circ }$, before declining gradually to $\sim \mathrm{0.8}$ as $\mathrm{\Delta }{\mathit{\varphi }}_{\mathrm{H}}$ continues to increase.

For each $\mathrm{\Delta }{\mathit{\varphi }}_{\mathrm{H}}$, the range of ${\underset{\mathrm{¯}}{\mathit{\epsilon }}}^s/{\mathit{\epsilon }}_{\mathrm{45}}^{\mathrm{b}}$ is limited, confirming the limited impact of $\mathit{\psi }$ and $t_{{\mathit{\varphi }}_{\mathrm{H}}}$ on the beam mean residual bias. However, this masks a much greater variation in the normalised residual bias for individual beams, ${\mathit{\epsilon }}_i^s/{\mathit{\epsilon }}_{\mathrm{45}}^{\mathrm{b}}$, as illustrated in panel (c), which shows the mean (black line) and the 25 % to 75 % (dark grey shading) and 5 % to 95 % (light grey shading) ranges for ${\mathit{\epsilon }}_i^s/{\mathit{\epsilon }}_{\mathrm{45}}^{\mathrm{b}}$ aggregated by $\mathrm{\Delta }{\mathit{\varphi }}_{\mathrm{H}}$. The potential variation between beams increases markedly over the range $\mathrm{50}{}^{\circ }\le \mathrm{\Delta }{\mathit{\varphi }}_{\mathrm{H}}\le \mathrm{200}$${}^{\circ }$ before being reduced, with maximum ${\mathit{\epsilon }}_i^s/{\mathit{\epsilon }}_{\mathrm{45}}^{\mathrm{b}}$ values exceeding 1.5 for $\mathrm{180}{}^{\circ }\le \mathrm{\Delta }{\mathit{\varphi }}_{\mathrm{H}}\le \mathrm{260}$${}^{\circ }$.

The vertical lines in panels (b) and (c) of Fig.  indicate the deployment 4 median (dotted line) and 90th percentile $\mathrm{\Delta }{\mathit{\varphi }}_{\mathrm{H}}$ values for the upper (grey) and middle (black) instruments from the observations described in Sect. . The results suggest that for these observations, the proportion of the potential bias likely to be retained is typically low, although under some circumstances it might exceed 50 % for the middle instrument.

Figure 9

Illustration of pitch oscillation in a sheared current for ${\mathit{\varphi }}_{\mathrm{P}}\left(\mathrm{0}\right)=\mathrm{0}$${}^{\circ }$, $\mathrm{\Delta }{\mathit{\varphi }}_{\mathrm{P}}=\mathrm{20}$${}^{\circ }$, and $t_{{\mathit{\varphi }}_{\mathrm{P}}}=\mathrm{30}$ s, with ${\mathit{\varphi }}_{\mathrm{H}}\left(t\right)=\mathit{\beta }$ and ${\mathit{\varphi }}_{\mathrm{R}}\left(t\right)=\mathrm{0}$${}^{\circ }$ for all $t$. Panel details as per Fig. .

[Figure omitted. See PDF]

4.3 Tilt variation example

Figure  illustrates the impact of oscillation on the pitch tilt axis for a sample scenario with constant heading and no roll, with all panels as described in Fig. . The initial pitch angle is ${\mathit{\varphi }}_{\mathrm{P}}\left(\mathrm{0}\right)=\mathrm{0}$${}^{\circ }$, the oscillation range $\mathrm{\Delta }{\mathit{\varphi }}_{\mathrm{P}}=\mathrm{20}$${}^{\circ }$, and the oscillation period $t_{{\mathit{\varphi }}_{\mathrm{P}}}=\mathrm{30}$ s. The heading is constant and aligned with the background flow, and there is no tilt on the roll axis, i.e. ${\mathit{\varphi }}_{\mathrm{H}}\left(t\right)=\mathit{\beta }$ and ${\mathit{\varphi }}_{\mathrm{R}}\left(t\right)=\mathrm{0}$${}^{\circ }$ for all $t$.

Panel (a) shows the sweep of the beams. At $t=\mathrm{0}$ s (circle marker), ${\mathit{\varphi }}_{\mathrm{P}}$ is 0${}^{\circ }$ and the instrument is vertical such that beams 1 and 2 (blue and red) are oriented normal to the current and their along-beam velocities are zero. As ${\mathit{\varphi }}_{\mathrm{P}}\left(t\right)$ becomes positive, beam 3 (yellow) is tilted towards the vertical so that its bins are higher in the water column than those in beam 4 (purple), as indicated by the position of square markers for the bin 30 positions after 2 s. This tilts beams 1 and 2 slightly upstream and $b$ becomes positive for all bins in both beams (red line overlying blue line), increasing to a positive maximum at $t_{{\mathit{\varphi }}_{\mathrm{P}}}/\mathrm{4}$ when ${\mathit{\varphi }}_{\mathrm{P}}\left(t\right)=\mathrm{\Delta }{\mathit{\varphi }}_{\mathrm{P}}/\mathrm{2}$ (just prior to the diamond marker at $t=\mathrm{8}$ s), then being reduced as ${\mathit{\varphi }}_{\mathrm{P}}$ declines so that both are zero again at $t_{{\mathit{\varphi }}_{\mathrm{P}}}/\mathrm{2}$, as shown in panel (b). As ${\mathit{\varphi }}_{\mathrm{P}}$ becomes negative, beams 1 and 2 are both tilted slightly downstream and $b$ becomes negative, reaching a maximum negative value at $\mathrm{3}{t}_{{\mathit{\varphi }}_{\mathrm{P}}}/\mathrm{4}$ when ${\mathit{\varphi }}_{\mathrm{P}}\left(t\right)=-\mathrm{\Delta }{\mathit{\varphi }}_{\mathrm{P}}/\mathrm{2}$ (close to the triangle marker at $t=\mathrm{22}$ s), before returning to zero after a full oscillation period. Consequently, for beams 1 and 2, $b$ is the same, oscillating in phase between positive and negative values with period $t_{{\mathit{\varphi }}_{\mathrm{P}}}$ and with the burst mean $⟨b_i⟩\approx \mathrm{0}$ m s${}^{-\mathrm{1}}$.

Beams 3 and 4 (yellow and purple) initially have a symmetrical orientation downstream and upstream, respectively, such that for any bin, $b_{\mathrm{3}}\left(\mathrm{0}\right)=-b_{\mathrm{4}}\left(\mathrm{0}\right)$. As ${\mathit{\varphi }}_{\mathrm{P}}$ becomes positive, the change in the relative orientation of beam 3 to the horizontal current reduces the magnitude of the along-beam velocity component $\left|b_{\mathrm{3}}\right|$, as shown in panel (b), despite the change in the bin depths increasing the local current speed. In contrast, beam 4 is tilted towards the horizontal, with the change in orientation resulting in $\left|b_{\mathrm{4}}\right|$ increasing, despite the reduction in the local current speed at the new bin depths. As the pitch oscillation continues, $b_{\mathrm{3}}$ and $b_{\mathrm{4}}$ vary in phase with each other, with $⟨b_i⟩\approx b_i\left(\mathrm{0}\right)$.

The slight differences in the depth ranges of the beams result in slight differences in $\mathit{\delta }{b}_i^{\prime }$ between the beams, as can be seen in panel (c). Whilst the variation is identical for beams 1 and 2 (red line overlying blue line), the $\left|\mathit{\delta }{b}_{\mathrm{3}}^{\prime }\right|$ maximum during the positive ${\mathit{\varphi }}_{\mathrm{P}}$ phase of the oscillation is larger than during the negative ${\mathit{\varphi }}_{\mathrm{P}}$ phase of the oscillation, with the situation reversed for beam 4. This is clearer in panel (d), which shows ${\left[\mathit{\delta }{b}_i^{\prime }\right]}^{\mathrm{2}}$. Beams 1 and 2 are identical, with the largest maxima and identical values during both the positive and negative ${\mathit{\varphi }}_{\mathrm{P}}$ phases, whilst the maxima for beams 3 and 4 are lower and differ between the phases such that the beam 3 values are larger during the positive ${\mathit{\varphi }}_{\mathrm{P}}$ phases and the beam 4 values during the negative ${\mathit{\varphi }}_{\mathrm{P}}$ phases.

The differences between beams 3 and 4 during the positive and negative phases of the oscillation are symmetric; therefore, the burst mean values used by the $D_{\mathrm{LL}}$ are identical, as shown in panel (e). Beams 3 and 4 yield identical results with ${\mathit{\epsilon }}_i^s/{\mathit{\epsilon }}_{\mathrm{45}}^{\mathrm{b}}$ values approximately 30 % lower than those for beams 1 and 2, for which the normalised residual bias as a result of the ADCP motion is $\sim \mathrm{0.1}$.

Oscillation about the roll axis, which in this scenario is oriented along the background flow, has no impact on $b_i$ for beams 1 and 2, which remain normal to the flow throughout the burst. The roll oscillation has a minimal impact on the vertical observation range for beams 3 and 4, resulting in a normalised residual bias in these beams of $\mathcal{O}{\mathrm{10}}^{-\mathrm{6}}$, highlighting the significance of the instrument orientation to the background flow for the impact of oscillation around the individual tilt axes.

4.4 Tilt variation scenarios

The potential impact of pitch and roll oscillations was evaluated for a sample of 500 000 scenarios based on the default configuration and sheared background flow. For each scenario, a constant heading angle was specified with ${\mathit{\varphi }}_{\mathrm{H}}\left(\mathrm{0}\right)$ selected at random (equal probability for each option) between 0 and 355${}^{\circ }$ at 5${}^{\circ }$ intervals and $\mathrm{\Delta }{\mathit{\varphi }}_{\mathrm{H}}=\mathrm{0}$${}^{\circ }$. Initial pitch angle, ${\mathit{\varphi }}_{\mathrm{P}}\left(\mathrm{0}\right)$, was randomly selected from the range $-\mathrm{10}$ to 10${}^{\circ }$ at 1${}^{\circ }$ intervals, pitch oscillation range $\mathrm{\Delta }{\mathit{\varphi }}_{\mathrm{P}}$ from the range $-\mathrm{20}$ to 20${}^{\circ }$ at 1${}^{\circ }$ intervals, with the sign indicating the initial rotation direction, and the pitch oscillation period $t_{{\mathit{\varphi }}_{\mathrm{P}}}$ randomly selected in the range 10 to 70 s. The initial roll angle, ${\mathit{\varphi }}_{\mathrm{R}}\left(\mathrm{0}\right)$, roll oscillation range, $\mathrm{\Delta }{\mathit{\varphi }}_{\mathrm{R}}$, and roll oscillation period, $t_{{\mathit{\varphi }}_{\mathrm{R}}}$, were randomly selected from the same ranges as the pitch equivalents, whilst the roll phase offset, $\mathit{\delta }{t}_{{\mathit{\varphi }}_{\mathrm{R}}}$, was randomly selected in the range 0 to 30 s. The ranges for each variable were chosen based on the sensor ranges and the observations described in Sect. , with the aim of covering the likely potential impacts.

Figure 10

Normalised residual bias distribution for scenarios with tilt oscillation. Each panel shows the mean (black line), 25 % to 75 % range (dark grey shading), and 5 % to 95 % range (light grey shading) for the beam-averaged normalised residual bias, ${\underset{\mathrm{¯}}{\mathit{\epsilon }}}^s/{\mathit{\epsilon }}_{\mathrm{45}}^{\mathrm{b}}$, together with the 95th percentile (dotted line with triangle markers) and maximum (grey line with square markers) individual beam-normalised residual bias, ${\mathit{\epsilon }}_i^s/{\mathit{\epsilon }}_{\mathrm{45}}^{\mathrm{b}}$ for scenarios aggregated by (a) the heading difference angle, $\mathit{\psi }$, (b) the sum of the absolute initial pitch and roll, $\left|{\mathit{\varphi }}_{\mathrm{P}}\right(\mathrm{0}\left)\right|+\left|{\mathit{\varphi }}_{\mathrm{R}}\right(\mathrm{0}\left)\right|$, and (c) the sum of the absolute pitch and roll angular oscillation ranges, $\left|\mathrm{\Delta }{\mathit{\varphi }}_{\mathrm{P}}\right|+\left|\mathrm{\Delta }{\mathit{\varphi }}_{\mathrm{R}}\right|$. The vertical lines in panel (c) are the deployment 4 median (dotted line) and 90th percentile (solid line) $\mathrm{\Delta }{\mathit{\varphi }}_{\mathrm{P}}+\mathrm{\Delta }{\mathit{\varphi }}_{\mathrm{R}}$ values for the upper (grey) and middle (black) instruments from the observations described in Sect. .

[Figure omitted. See PDF]

Figure  shows the mean (black line), 25 % to 75 % range (dark grey shading), and 5 % to 95 % range (light grey shading) for the beam-averaged normalised residual bias ${\underset{\mathrm{¯}}{\mathit{\epsilon }}}^s/{\mathit{\epsilon }}_{\mathrm{45}}^{\mathrm{b}}$, together with the 95th percentile (dotted line with triangle markers) and maximum (grey line with square markers) individual beam-normalised residual bias ${\mathit{\epsilon }}_i^s/{\mathit{\epsilon }}_{\mathrm{45}}^{\mathrm{b}}$ for scenarios aggregated by (a) the heading offset angle to the background flow $\mathit{\psi }$, (b) the sum of the absolute values of the initial tilt angles $\left|{\mathit{\varphi }}_{\mathrm{P}}\right(\mathrm{0}\left)\right|+\left|{\mathit{\varphi }}_{\mathrm{R}}\right(\mathrm{0}\left)\right|$, and (c) the sum of the absolute values of the tilt oscillation ranges $\left|\mathrm{\Delta }{\mathit{\varphi }}_{\mathrm{P}}\right|+\left|\mathrm{\Delta }{\mathit{\varphi }}_{\mathrm{R}}\right|$.

Panel (a) illustrates how the symmetry of the ADCP beam geometry is reflected in the impact of the instrument orientation relative to the background flow. The mean ${\underset{\mathrm{¯}}{\mathit{\epsilon }}}^s/{\mathit{\epsilon }}_{\mathrm{45}}^{\mathrm{b}}$ is effectively constant (mean 0.023) across all $\mathit{\psi }$, whilst the range of the beam average values (light grey shading) is largest when the heading is such that one of the beams is aligned with the background flow, i.e. $\mathit{\psi }$ is 0, $\pm \mathrm{90}$, or $\pm \mathrm{180}$${}^{\circ }$, and smallest when all beams are at 45${}^{\circ }$ to the background flow, i.e. $\mathit{\psi }$ is $\pm \mathrm{45}$ or $\pm \mathrm{135}$${}^{\circ }$.

There is a marked contrast between the 95th percentile of the individual beam-normalised residual bias ${\mathit{\epsilon }}_i^s/{\mathit{\epsilon }}_{\mathrm{45}}^{\mathrm{b}}$ (dotted line with triangle marker), which closely tracks that of the beam-averaged values, and the beam maximum (grey line with square marker). They vary in anti-phase, with maximum ${\mathit{\epsilon }}_i^s/{\mathit{\epsilon }}_{\mathrm{45}}^{\mathrm{b}}$ values of $\sim \mathrm{0.3}$ occurring with $\mathit{\psi }\sim \pm \mathrm{45}$ or $\pm \mathrm{135}$${}^{\circ }$.

Panel (b) shows that the mean and range of ${\underset{\mathrm{¯}}{\mathit{\epsilon }}}^s/{\mathit{\epsilon }}_{\mathrm{45}}^{\mathrm{b}}$ exhibit minimal dependence on the mean tilt, as indicated by the sum of the initial tilt angles $\left|{\mathit{\varphi }}_{\mathrm{P}}\right(\mathrm{0}\left)\right|+\left|{\mathit{\varphi }}_{\mathrm{R}}\right(\mathrm{0}\left)\right|$, again recognising that the specified tilt oscillation means that $⟨{\mathit{\varphi }}_{\mathrm{P}}⟩\approx {\mathit{\varphi }}_{\mathrm{P}}\left(\mathrm{0}\right)$ and $⟨{\mathit{\varphi }}_{\mathrm{R}}⟩\approx {\mathit{\varphi }}_{\mathrm{R}}\left(\mathrm{0}\right)$. The 5 % to 95 % range actually narrows slightly as the mean tilt increases. The 95th percentile of the individual beam ${\mathit{\epsilon }}_i^s/{\mathit{\epsilon }}_{\mathrm{45}}^{\mathrm{b}}$ values is also effectively constant, whilst there is a gradual increase in the maximum ${\mathit{\epsilon }}_i^s/{\mathit{\epsilon }}_{\mathrm{45}}^{\mathrm{b}}$ values as $\left|{\mathit{\varphi }}_{\mathrm{P}}\right(\mathrm{0}\left)\right|+\left|{\mathit{\varphi }}_{\mathrm{R}}\right(\mathrm{0}\left)\right|$ increases from 0 to 6${}^{\circ }$, above which it is relatively constant.

Panel (c) indicates that for the scenarios examined, the residual bias is primarily determined by the total absolute oscillation range, $\left|\mathrm{\Delta }{\mathit{\varphi }}_{\mathrm{P}}\right|+\left|\mathrm{\Delta }{\mathit{\varphi }}_{\mathrm{R}}\right|$. The mean ${\underset{\mathrm{¯}}{\mathit{\epsilon }}}^s/{\mathit{\epsilon }}_{\mathrm{45}}^{\mathrm{b}}$ is $\sim \mathrm{0}$ for $\left|\mathrm{\Delta }{\mathit{\varphi }}_{\mathrm{P}}\right|+\left|\mathrm{\Delta }{\mathit{\varphi }}_{\mathrm{R}}\right|\le \mathrm{15}$${}^{\circ }$, gradually increasing to a maximum of $\sim \mathrm{0.09}$ (black line). The range of ${\underset{\mathrm{¯}}{\mathit{\epsilon }}}^s/{\mathit{\epsilon }}_{\mathrm{45}}^{\mathrm{b}}$ values is narrow for all $\left|\mathrm{\Delta }{\mathit{\varphi }}_{\mathrm{P}}\right|+\left|\mathrm{\Delta }{\mathit{\varphi }}_{\mathrm{R}}\right|$ options. The 95th percentile of the individual beam ${\mathit{\epsilon }}_i^s/{\mathit{\epsilon }}_{\mathrm{45}}^{\mathrm{b}}$ values closely tracks that of ${\underset{\mathrm{¯}}{\mathit{\epsilon }}}^s/{\mathit{\epsilon }}_{\mathrm{45}}^{\mathrm{b}}$ for $\left|\mathrm{\Delta }{\mathit{\varphi }}_{\mathrm{P}}\right|+\left|\mathrm{\Delta }{\mathit{\varphi }}_{\mathrm{R}}\right|\le \mathrm{20}$${}^{\circ }$, above which it increases at a slightly higher rate. This is also reflected in the beam maximum ${\mathit{\epsilon }}_i^s/{\mathit{\epsilon }}_{\mathrm{45}}^{\mathrm{b}}$ values, which grow at an increasing rate, exceeding 0.3 for the extreme scenarios with $\left|\mathrm{\Delta }{\mathit{\varphi }}_{\mathrm{P}}\right|+\left|\mathrm{\Delta }{\mathit{\varphi }}_{\mathrm{R}}\right|$ approaching 40${}^{\circ }$.

The vertical lines in panel (c) are the deployment 4 median (dotted line) and 90th percentile (solid line) $\mathrm{\Delta }{\mathit{\varphi }}_{\mathrm{P}}+\mathrm{\Delta }{\mathit{\varphi }}_{\mathrm{R}}$ values for the upper (grey) and middle (black) instruments from the observations described in Sect. . The results suggest that for these observations, oscillation on the tilt axes is unlikely to result in the beam average retaining a significant fraction of the potential bias, although for individual beams it may exceed 10 % in some circumstances.

4.5 Effectiveness of the modified regression method

identified that the orbital velocities due to surface waves contribute a periodic velocity component that varies between bins due to their spatial separation, leading to residual non-turbulent velocity differences in the structure function and biased $\mathit{\epsilon }$ estimates. Over a limited spatial range, the velocity difference between bins varies linearly with separation distance, resulting in a contribution to the second-order structure function with an $r^{\mathrm{2}}$ length-scale dependency.

As described in Sect. , any residual structure function contribution due to the motion of the ADCP in the presence of linear shear will also exhibit an $r^{\mathrm{2}}$ length-scale dependency. This suggests that the modified regression including terms for both $r^{\frac{\mathrm{2}}{\mathrm{3}}}$ and $(r^{\frac{\mathrm{2}}{\mathrm{3}}}{)}^{\mathrm{3}}$, as per Eq. (), should also be effective in isolating any non-turbulent contribution due to shear from the genuine turbulence signal.

This was tested on the synthesised data (with or without the deduction of the burst mean) and was found to completely eliminate the bias, yielding $\mathit{\epsilon }$ values of $\mathcal{O}{\mathrm{10}}^{-\mathrm{30}}$ W kg${}^{-\mathrm{1}}$ or less, reflecting the numerical precision of the calculations.

The synthesised data represent a pure “bias” signal and are therefore optimised to be identified and isolated. The effectiveness of the modified method with real observations affected by ADCP motion in a sheared flow is likely to be determined by the noise in the signal and the choice of $r_{\max }$. Furthermore, since the same term in the modified regression is used to isolate both the bias contribution due to surface waves and that due to residual shear, it is not possible to distinguish between these factors in interpreting the impact of applying the modified regression to real observations when both may be relevant.

5 Discussion

The standard structure function methodology assumes that the along-beam velocities observed by an ADCP can be decomposed into a component due to the background flow and the time-varying turbulent velocities required to calculate $\mathit{\epsilon }$. Deducting the mean or linear trend over a burst of observations for each bin therefore removes the component due to the background flow, including any non-turbulent velocity differences between bins due to shear. For this assumption to be valid, there must be no spatially varying periodic non-turbulent velocity contribution to the observed velocity, such as that due to surface waves or, as considered here, due to the motion of the ADCP in a sheared background flow.

If the orientation of the ADCP varies, the burst mean velocity in any bin unavoidably underestimates the background flow contribution in some profiles and overestimates it in others. If the background flow is sheared, the residual velocity when the burst mean or linear trend is deducted will include a proportion of the associated non-turbulent velocity differences between bins.

The potential contribution to the second-order structure function if the velocity differences due to linear shear in the background flow were wholly retained in the residual velocity is shown here to scale with the square of both the shear and the separation distance; see Eq. (). The potential bias will therefore scale as the cube of the shear and will be sensitive to both the choice of the maximum separation distance over which the structure function is evaluated and the ADCP bin size (which determines the number of resolved separation distances).

Data from long-term deployments of three ADCPs mounted inline on a buoyancy-tensioned mooring demonstrate the instruments oscillating in heading, pitch, and roll. The heading variation was found to vary between fewer larger-amplitude oscillations when the background flow is slowest and a higher number of smaller-amplitude oscillations as the background flow speed increased. The background flow speed also directly influenced the mean tilt angle for the instruments as the drag determines the shape of the mooring. Surface waves had some influence on heading variation; however, the impact was most apparent in the range of the tilt oscillation. There was also evidence that the way in which the ADCP was mounted influenced the movement, with the instruments in spherical syntactic buoys subject to less motion than those in an open frame.

Synthesised along-beam velocity data based on a standard TRDI WorkHorse ADCP geometry were used to evaluate the impact of instrument motion in a linearly sheared flow. The residual bias was normalised by the potential bias for the defined geometry, background flow, and with all beams having the same relative orientation to the flow.

Based on a wide range of synthesised scenarios, the normalised residual bias was found to be primarily determined by the oscillation angular range for both heading and instrument tilt.

Testing indicated that the normalised residual bias becomes increasingly significant for heading angular oscillation ranges exceeding 50${}^{\circ }$, with the possibility of the full potential bias being retained in one or more beams if the angular range exceeded 140${}^{\circ }$. The frequency of occurrence of heading oscillations exceeding 50${}^{\circ }$ in the observations examined was dependent on the instrument mounting, but it affected more than 50 % of observations for the instrument mounted in an open frame during some deployments. Furthermore, since the heading oscillation was unconstrained, angular variations of over 360${}^{\circ }$ occasionally occurred.

Oscillation on the tilt axes is inherently constrained by the tension in the mooring; therefore, the potential angular range is limited. The synthesised scenarios suggest that the beam-averaged normalised residual bias due to tilt oscillation will reach 10 % only under exceptional circumstances. However, the maximum residual bias for an individual beam, which increases with the total of the pitch and roll angular ranges, can reach 30 % of the potential bias under exceptional circumstances.

The velocity difference between bins due to shear, retained in the along-beam velocity as a consequence of the ADCP motion, varies linearly with separation distance. This is consistent with that arising from the spatial gradient of the orbital velocities forced by surface gravity waves, suggesting that the modified regression in Eq. (), as described by , should be effective in isolating the turbulence signal from any bias. This was confirmed when the modified regression was applied to the synthesised scenarios described in Sect. , with the potential bias being completely eliminated. The results suggest that the modified regression may be useful in a wider range of circumstances than removing bias due to surface waves, isolating all non-turbulent velocity differences that scale linearly with separation distance, although without distinguishing between possible sources.

This analysis suggests that under most circumstances the motion of a tethered ADCP is unlikely to be a significant source of errors in $\mathit{\epsilon }$ estimates derived using the standard structure function methodology. However, since the potential bias scales with the cube of the shear and depends on factors such as the bin size and the length scale over which the structure function is evaluated, there may be circumstances in which it is significant. Furthermore, since the level of retained bias is dependent on the motion of the ADCP, it is relevant to identify this as an issue for consideration as part of both the deployment planning and the data quality assurance and analysis. The following suggestions may therefore be of interest to other researchers.

• Mooring design. Mounting the ADCP in a streamlined buoy designed to maintain a fixed orientation relative to the background current is recommended for all deployments on a tethered mooring. If that is not an option, mounting the ADCP in a spherical buoy is likely to result in less motion than using an open frame.

• ADCP configuration. Ensure that the instrument orientation sensors (heading, pitch, and roll) are working properly and that the instrument is configured to save the data at the same temporal resolution as the velocity profiles.

• Initial QA. Check for periodic variations in heading, pitch or roll to determine whether the ADCP was subject to significant motion during the observation bursts. In particular, evaluate the heading angular variation range $\mathrm{\Delta }{\mathit{\varphi }}_{\mathrm{H}}$, with $\mathrm{\Delta }{\mathit{\varphi }}_{\mathrm{H}}\ge \mathrm{50}$${}^{\circ }$ suggested as a threshold above which the possibility of bias should be considered.

• Initial QA. Check for periodic variation in the along-beam velocity data collected. One option is to examine the burst variance of the along-beam velocity and check for any monotonic trend in the variance between bins, which may indicate a non-turbulent contribution and potential cause of bias.

• Shear. Convert the along-beam velocity data to Earth coordinates and determine the level of shear. This can be used to determine the maximum potential bias by computing the sheared structure function $D_{\mathrm{LL}}^{\mathrm{b}}$ as per Eq. () based on the bin size and beam angle and then calculating the potential bias ${\mathit{\epsilon }}^{\mathrm{b}}$ for the proposed $r_{\max }$.

• Structure function QA. Check for non-linearity of $D_{\mathrm{LL}}$ versus $r^{\mathrm{2}/\mathrm{3}}$. This is perhaps most easily achieved by examining the sensitivity of $\mathit{\epsilon }$ to increasing $r_{\max }$, with an increasing trend probably indicating a non-turbulent contribution to $D_{\mathrm{LL}}$ and therefore a bias in the calculated $\mathit{\epsilon }$ values.

• Structure function QA. Test whether $\mathit{\epsilon }$ values are more independent of $r_{\max }$ when using the modified regression in Eq. (). If so, this suggests a non-turbulent contribution to $D_{\mathrm{LL}}$, but care should be taken to determine the source of the non-turbulent contribution and verify that the associated velocity difference between bins varies linearly with separation distance before assuming the modified method is applicable.

Appendix A Celtic Sea turbulence mooring

The moorings were deployed at a site in the central Celtic Sea (latitude 49${}^{\circ }$ 24${}^{\prime }$ N, longitude 8${}^{\circ }$36${}^{\prime }$ W). The site has a nominal depth of 145 m and is more than 200 km from any coast and over 125 km from the shelf break.

Table A1

Turbulence mooring deployment periods.

Dep.	Recovery cruise	Deployment date	Recovery date	Bursts returned by instrument
				upper	middle	lower
1	JC105	27 March 2014	19 June 2014	5799${}^{\mathrm{a}}$	1621${}^{\mathrm{b}}$	5799${}^{\mathrm{a}}$
2	DY026	22 June 2014	21 August 2014	4332	3695${}^{\mathrm{c}}$	4333
3	DY018	22 August 2014	20 November 2014	6472	6472	6473
4	DY029	22 November 2014	4 April 2015	9571	9572	9571
5	DY033	11 April 2015	25 July 2015	7568	7567	7568

${}^{\mathrm{a}}$ No data after 15 June 2014 – memory full. ${}^{\mathrm{b}}$ No data after 18 April 2014 – instrument stopped logging. ${}^{\mathrm{c}}$ No data between 8 and 17 July 2014 – instrument stopped logging.

The overall deployment period was from late March 2014 to late July 2015, during which time it was serviced four times, with the interval between recovery and redeployment varying between 1 and 7 d. The same instruments were used for each period in the same mooring arrangement and with the same sampling configuration. Table  shows the dates for the individual deployment periods together with the associated number of observation bursts returned by each instrument.

Table A2

Heading statistics by deployment and instrument. Number of bursts, $n_{\mathrm{obs}}$, and mean instrument depth, $\stackrel{\mathrm{‾}}{z}$ m, are shown. For heading range, $\mathrm{\Delta }{\mathit{\varphi }}_{\mathrm{H}}$, the following are indicated: the mean, $\stackrel{\mathrm{‾}}{\mathrm{\Delta }{\mathit{\varphi }}_{\mathrm{H}}}$; 10th, 50th, and 90th percentiles; and the percentage of bursts with $\mathrm{\Delta }{\mathit{\varphi }}_{\mathrm{H}}\ge \mathrm{360}$${}^{\circ }$. For oscillation count per burst, $n_{{\mathit{\varphi }}_{\mathrm{H}}}$, the following are indicated: the mean, $\stackrel{\mathrm{‾}}{n_{{\mathit{\varphi }}_{\mathrm{H}}}}$; percentage of bursts with $n_{{\mathit{\varphi }}_{\mathrm{H}}}\le \mathrm{1}$; and the 50th and 90th percentiles.

Dep.	Inst.	$n_{\mathrm{obs}}$	$\stackrel{\mathrm{‾}}{z}$	$\mathrm{\Delta }{\mathit{\varphi }}_{\mathrm{H}}$					$n_{{\mathit{\varphi }}_{\mathrm{H}}}$
				$\stackrel{\mathrm{‾}}{\mathrm{\Delta }{\mathit{\varphi }}_{\mathrm{H}}}$	10 %	50 %	90 %	$\ge \mathrm{360}$${}^{\circ }$	$\stackrel{\mathrm{‾}}{n_{{\mathit{\varphi }}_{\mathrm{H}}}}$	$\le \mathrm{1}$	50 %	90 %
1	upper	5799	19.2	36.2	15.2	25.8	68.6	0.10 %	11.1	1.10 %	11	18
	middle	1621	32.9	74.4	39.6	65.9	123.5	0.00 %	28.3	0.37 %	26	49
	lower	5799	49.4	22.9	10.9	17.9	37.6	0.10 %	10.2	1.21 %	10	17
2	upper	4332	19.6	21.1	12.5	19.2	30.7	0.02 %	19.1	0.46 %	20	27
	middle	3695	32.9	64.6	27.7	52.1	118.5	0.03 %	22.7	2.49 %	22	42
	lower	4333	50.0	18.7	10.5	15.8	26.4	0.16 %	10.4	2.86 %	10	18
3	upper	6472	19.7	50.6	19.7	38.9	89.7	0.20 %	9.7	4.64 %	9	18
	middle	6472	33.2	98.7	39.5	84.9	175.4	0.59 %	17.8	1.44 %	18	25
	lower	6473	50.4	30.0	14.7	23.4	48.1	0.14 %	11.6	2.53 %	11	20
4	upper	9571	22.3	48.9	23.0	39.1	85.7	0.07 %	14.9	0.72 %	15	23
	middle	9572	35.7	80.0	29.2	59.5	154.6	0.90 %	20.7	1.08 %	22	27
	lower	9571	50.8	41.6	15.8	27.6	79.3	0.22 %	8.5	2.60 %	8	15
5	upper	7568	19.5	30.8	15.6	24.9	49.8	0.05 %	10.8	1.36 %	10	18
	middle	7567	33.1	54.8	24.1	44.3	96.9	0.09 %	23.7	0.94 %	23	34
	lower	7568	50.3	20.8	10.8	16.5	30.8	0.11 %	9.8	1.88 %	9	17

A1 Heading

Table  provides information on the heading variation for each instrument and each deployment, together with the number of observation bursts, $n_{\mathrm{obs}}$, and the mean depth, $\stackrel{\mathrm{‾}}{z}$ (m). The burst maximum heading variation, $\mathrm{\Delta }{\mathit{\varphi }}_{\mathrm{H}}$, is evaluated as the absolute difference between the minimum and maximum ${\mathit{\varphi }}_{\mathrm{H}}$ expressed on a continuous basis such that if the instrument completes a full rotation during the burst, $\mathrm{\Delta }{\mathit{\varphi }}_{\mathrm{H}}\ge \mathrm{360}$${}^{\circ }$. The table shows $\stackrel{\mathrm{‾}}{\mathrm{\Delta }{\mathit{\varphi }}_{\mathrm{H}}}$, which is the mean $\mathrm{\Delta }{\mathit{\varphi }}_{\mathrm{H}}$ for the instrument over the deployment period, together with the 10th, 50th, and 90th percentile values and the percentage of bursts for which $\mathrm{\Delta }{\mathit{\varphi }}_{\mathrm{H}}\ge \mathrm{360}$${}^{\circ }$.

The number of heading oscillations per burst, $n_{{\mathit{\varphi }}_{\mathrm{H}}}$, was evaluated as the number of times ${\mathit{\varphi }}_{\mathrm{H}}$ increased above the burst mean heading, $⟨{\mathit{\varphi }}_{\mathrm{H}}⟩$, such that ${\mathit{\varphi }}_{\mathrm{H}}-⟨{\mathit{\varphi }}_{\mathrm{H}}⟩$ changed from negative to positive. The table shows $\stackrel{\mathrm{‾}}{n_{{\mathit{\varphi }}_{\mathrm{H}}}}$, which is the mean across all bursts, together with the percentage of bursts for which $n_{{\mathit{\varphi }}_{\mathrm{H}}}\le \mathrm{1}$ and the 50th and 90th percentile $n_{{\mathit{\varphi }}_{\mathrm{H}}}$ values.

Examination of a sample of bursts for which $n_{{\mathit{\varphi }}_{\mathrm{H}}}\le \mathrm{1}$ indicated that they were characterised by a significant step change in the heading, resulting in two distinct sub-periods during the burst. Despite ${\mathit{\varphi }}_{\mathrm{H}}$ oscillating about the relevant mean during each sub-period, there was just a single crossing of $⟨{\mathit{\varphi }}_{\mathrm{H}}⟩$, resulting in $n_{{\mathit{\varphi }}_{\mathrm{H}}}$ being 0 or 1.

Figure A1

Cumulative probability of (a)–(c) burst heading range, $\mathrm{\Delta }{\mathit{\varphi }}_{\mathrm{H}}$, and (d)–(f) mean number of oscillations per burst, $n_{{\mathit{\varphi }}_{\mathrm{H}}}$, by instrument and deployment, as per legend in panel (a).

[Figure omitted. See PDF]

The heading variation is further illustrated in Fig. . Panels (a)–(c) show the cumulative distribution of $\mathrm{\Delta }{\mathit{\varphi }}_{\mathrm{H}}$, with the line colour indicating the deployment as per the legend in panel (a) and the embedded table in each panel showing the percentage of bursts per deployment when $\mathrm{\Delta }{\mathit{\varphi }}_{\mathrm{H}}\ge \mathrm{180}$ and 360${}^{\circ }$. Panels (d)–(f) show the cumulative distribution of $n_{{\mathit{\varphi }}_{\mathrm{H}}}$, with the embedded tables showing the percentage of bursts per deployment when $n_{{\mathit{\varphi }}_{\mathrm{H}}}\ge \mathrm{50}$. Panels (a) and (d) relate to the upper instrument, (b) and (e) the middle instrument, and (c) and (f) the lower instrument.

The middle instrument is subject to significantly higher levels of heading variation in terms of both the range of the angular variation and the number of oscillations per burst. This is interpreted as being a consequence of the different housing used for the instruments in the mooring – the upper and lower instruments are embedded within a spherical syntactic buoy, whilst the middle instrument was in an open frame.

The same housings were used for each deployment, so the differences in the $\mathrm{\Delta }{\mathit{\varphi }}_{\mathrm{H}}$ and $n_{{\mathit{\varphi }}_{\mathrm{H}}}$ distributions between deployments for the individual instruments must arise either from performance differences of mooring elements, e.g. swivels or wires, or from differing environmental conditions.

A2 Tilt

Pitch and roll, ${\mathit{\varphi }}_{\mathrm{P}}$ and ${\mathit{\varphi }}_{\mathrm{R}}$, typically have a constant sign throughout an observation burst, with the burst mean values $⟨{\mathit{\varphi }}_{\mathrm{P}}⟩$ and $⟨{\mathit{\varphi }}_{\mathrm{R}}⟩$ tending to have a consistent sign throughout a deployment. This indicates that the initial orientation of the instruments in the mooring results in a preferred orientation relative to the plane of the mooring, which persists throughout the deployment with limited variation, despite the rotation of the mooring with the tide.

Table A3

Pitch statistics by deployment and instrument. For the absolute burst mean pitch, $|⟨{\mathit{\varphi }}_{\mathrm{P}}⟩|$, the deployment mean, $\stackrel{\mathrm{‾}}{|⟨{\mathit{\varphi }}_{\mathrm{P}}⟩|}$, and the percentage of bursts with $|⟨{\mathit{\varphi }}_{\mathrm{P}}⟩|\ge \mathrm{5}$ and 10${}^{\circ }$ are indicated. For the pitch burst range, $\mathrm{\Delta }{\mathit{\varphi }}_{\mathrm{P}}$, the deployment mean, $\stackrel{\mathrm{‾}}{\mathrm{\Delta }{\mathit{\varphi }}_{\mathrm{P}}}$, as well as the 10th, 50th, and 90th percentiles are indicated. For the oscillations per burst, $n_{{\mathit{\varphi }}_{\mathrm{P}}}$, the deployment mean, $\stackrel{\mathrm{‾}}{n_{{\mathit{\varphi }}_{\mathrm{P}}}}$, as well as the 10th, 50th, and 90th percentiles are indicated.

Dep.	Inst.	$|⟨{\mathit{\varphi }}_{\mathrm{P}}⟩|$			$\mathrm{\Delta }{\mathit{\varphi }}_{\mathrm{P}}$				$n_{{\mathit{\varphi }}_{\mathrm{P}}}$
		$\stackrel{\mathrm{‾}}{|⟨{\mathit{\varphi }}_{\mathrm{P}}⟩|}$	$\ge \mathrm{5}$${}^{\circ }$	$\ge \mathrm{10}$${}^{\circ }$	$\stackrel{\mathrm{‾}}{\mathrm{\Delta }{\mathit{\varphi }}_{\mathrm{P}}}$	10 %	50 %	90 %	$\stackrel{\mathrm{‾}}{n_{{\mathit{\varphi }}_{\mathrm{P}}}}$	10 %	50 %	90 %
1	upper	1.3	0.1 %	0.00 %	4.5	2.1	4.0	7.4	34.8	29	34	41
	middle	2.8	7.6 %	0.00 %	6.8	3.3	6.1	11.6	35.5	26	33	50
	lower	3.1	17.9 %	0.78 %	1.6	0.9	1.4	2.4	32.4	19	29	50
2	upper	3.7	16.8 %	0.00 %	3.4	1.6	3.0	5.6	34.5	27	34	42
	middle	2.7	12.5 %	1.62 %	3.7	1.1	2.6	7.6	28.7	11	29	45
	lower	3.4	18.0 %	0.02 %	1.2	0.6	1.0	2.0	29.8	15	27	48
3	upper	2.4	11.6 %	0.83 %	5.0	1.9	4.4	8.8	32.4	27	32	39
	middle	1.9	8.7 %	1.59 %	5.5	2.0	4.8	9.8	28.7	17	28	39
	lower	2.7	14.7 %	1.79 %	2.1	0.8	1.8	3.7	26.6	17	25	38
4	upper	2.6	6.9 %	0.00 %	7.6	3.7	7.0	12.0	29.0	25	29	33
	middle	3.3	24.7 %	2.84 %	5.6	2.3	4.6	10.2	30.8	23	30	40
	lower	3.6	25.3 %	1.49 %	3.0	1.4	2.6	5.0	24.0	16	23	33
5	upper	2.2	8.9 %	0.01 %	4.6	2.2	4.1	7.5	33.4	27	33	40
	middle	2.6	14.3 %	1.94 %	4.0	1.7	3.2	7.2	35.6	24	34	51
	lower	2.7	15.8 %	1.41 %	1.6	0.8	1.4	2.8	29.4	17	27	44

Table A4

Roll statistics by deployment and instrument. For the absolute burst mean roll, $|⟨{\mathit{\varphi }}_{\mathrm{R}}⟩|$, the deployment mean, $\stackrel{\mathrm{‾}}{|⟨{\mathit{\varphi }}_{\mathrm{R}}⟩|}$, and the percentage of bursts with $|⟨{\mathit{\varphi }}_{\mathrm{R}}⟩|\ge \mathrm{5}$ and 10${}^{\circ }$ are indicated. For the roll burst range, $\mathrm{\Delta }{\mathit{\varphi }}_{\mathrm{R}}$, the deployment mean, $\stackrel{\mathrm{‾}}{\mathrm{\Delta }{\mathit{\varphi }}_{\mathrm{R}}}$, as well as the 10th, 50th, and 90th percentiles are indicated. For the oscillations per burst, $n_{{\mathit{\varphi }}_{\mathrm{R}}}$, the deployment mean, $\stackrel{\mathrm{‾}}{n_{{\mathit{\varphi }}_{\mathrm{R}}}}$, as well as the 10th, 50th, and 90th percentiles are indicated.

Dep.	Inst.	$|⟨{\mathit{\varphi }}_{\mathrm{R}}⟩|$			$\mathrm{\Delta }{\mathit{\varphi }}_{\mathrm{R}}$				$n_{{\mathit{\varphi }}_{\mathrm{R}}}$
		$\stackrel{\mathrm{‾}}{|⟨{\mathit{\varphi }}_{\mathrm{R}}⟩|}$	$\ge \mathrm{5}$${}^{\circ }$	$\ge \mathrm{10}$${}^{\circ }$	$\stackrel{\mathrm{‾}}{\mathrm{\Delta }{\mathit{\varphi }}_{\mathrm{R}}}$	10 %	50 %	90 %	$\stackrel{\mathrm{‾}}{n_{{\mathit{\varphi }}_{\mathrm{R}}}}$	10 %	50 %	90 %
1	upper	0.8	0.0 %	0.00 %	4.9	2.5	4.6	7.5	34.0	28	33	41
	middle	4.6	38.3 %	3.95 %	4.6	2.5	4.3	7.2	36.8	27	34	52
	lower	1.5	2.6 %	0.00 %	1.6	0.8	1.3	2.5	34.9	23	31	53
2	upper	1.8	4.6 %	0.07 %	3.2	1.6	2.9	5.2	35.8	28	36	44
	middle	2.4	10.7 %	1.30 %	3.8	1.2	2.8	7.9	28.3	10	30	44
	lower	4.3	29.5 %	4.08 %	1.2	0.6	1.0	2.0	25.0	8	23	44
3	upper	2.2	0.1 %	0.00 %	5.9	2.2	5.4	10.3	31.1	25	30	39
	middle	2.5	10.9 %	1.38 %	5.6	1.8	4.8	10.2	28.2	17	28	39
	lower	1.6	4.2 %	0.00 %	2.2	0.9	1.9	3.8	29.0	20	26	41
4	upper	3.5	19.7 %	0.01 %	6.8	3.5	6.4	10.8	29.6	25	29	34
	middle	2.1	9.3 %	0.42 %	6.0	2.7	5.2	10.4	30.6	24	30	40
	lower	3.2	16.8 %	2.83 %	3.3	1.3	2.8	5.6	25.0	18	24	34
5	upper	4.1	28.6 %	0.89 %	4.4	2.0	3.9	7.5	34.0	28	34	41
	middle	3.6	22.6 %	3.86 %	4.3	1.7	3.5	7.8	35.4	24	34	50
	lower	4.0	29.1 %	1.02 %	1.5	0.7	1.3	2.7	30.8	20	29	44

Tables  and provide summary statistics for the pitch and roll data for each instrument during each of the deployments. For the absolute burst mean tilts, $|⟨{\mathit{\varphi }}_{\mathrm{P}}⟩|$ and $|⟨{\mathit{\varphi }}_{\mathrm{R}}⟩|$, the tables show the deployment mean, $\stackrel{\mathrm{‾}}{|⟨{\mathit{\varphi }}_{\mathrm{P}}⟩|}$ and $\stackrel{\mathrm{‾}}{|⟨{\mathit{\varphi }}_{\mathrm{R}}⟩|}$, together with the percentage of bursts $\ge \mathrm{5}$ and $\ge \mathrm{10}$${}^{\circ }$. For the burst oscillation ranges, $\mathrm{\Delta }{\mathit{\varphi }}_{\mathrm{P}}$ and $\mathrm{\Delta }{\mathit{\varphi }}_{\mathrm{R}}$, and the burst oscillation counts, $n_{{\mathit{\varphi }}_{\mathrm{P}}}$ and $n_{{\mathit{\varphi }}_{\mathrm{R}}}$, the tables show the deployment mean together with the 10th, 50th, and 90th percentiles. $\mathrm{\Delta }{\mathit{\varphi }}_{\mathrm{P}}$ and $\mathrm{\Delta }{\mathit{\varphi }}_{\mathrm{R}}$ are evaluated as the absolute difference between the burst minimum and maximum ${\mathit{\varphi }}_{\mathrm{P}}$ and ${\mathit{\varphi }}_{\mathrm{R}}$, respectively, and $n_{{\mathit{\varphi }}_{\mathrm{P}}}$ and $n_{{\mathit{\varphi }}_{\mathrm{R}}}$ are evaluated as the number of instances during a burst when the tilt increases through the burst mean, e.g. when ${\mathit{\varphi }}_{\mathrm{P}}-⟨{\mathit{\varphi }}_{\mathrm{P}}⟩$ changes from negative to positive.

The non-zero values for $\stackrel{\mathrm{‾}}{|⟨{\mathit{\varphi }}_{\mathrm{P}}⟩|}$ and $\stackrel{\mathrm{‾}}{|⟨{\mathit{\varphi }}_{\mathrm{R}}⟩|}$ suggest that the instruments were typically tilted from the vertical during a burst. The percentage of bursts with high $|⟨{\mathit{\varphi }}_{\mathrm{P}}⟩|$ or $|⟨{\mathit{\varphi }}_{\mathrm{R}}⟩|$ tends to be highest for the lower instrument and lowest for the upper instrument, consistent with the mooring exhibiting a catenary shape due to lateral loading.

The deployment mean burst ranges, $\stackrel{\mathrm{‾}}{\mathrm{\Delta }{\mathit{\varphi }}_{\mathrm{P}}}$ and $\stackrel{\mathrm{‾}}{\mathrm{\Delta }{\mathit{\varphi }}_{\mathrm{R}}}$, tend to decline with instrument depth and to vary in a consistent manner between deployments, being highest during the autumn and winter deployments 3 and 4 and lowest during the summer deployment 2.

The oscillation frequency, as indicated by $\stackrel{\mathrm{‾}}{n_{{\mathit{\varphi }}_{\mathrm{P}}}}$ and $\stackrel{\mathrm{‾}}{n_{{\mathit{\varphi }}_{\mathrm{R}}}}$, is consistent across all instruments and deployments, being higher than the equivalent $\stackrel{\mathrm{‾}}{n_{{\mathit{\varphi }}_{\mathrm{H}}}}$, particularly for the upper and lower instruments.

Figure A2

Cumulative probability of (a)–(c) burst tilt range, $\mathrm{\Delta }\mathit{\alpha }$, and (d)–(f) mean number of tilt oscillations per burst, $n_{\mathit{\alpha }}$, by instrument and deployment, with line colour indicating the deployment as shown in panel (a); tables in panels (a)–(c) show the percentage of bursts when $\mathrm{\Delta }\mathit{\alpha }$ exceeded 5 and 10${}^{\circ }$; tables in panels (d)–(f) show the percentage of bursts when $n_{\mathit{\alpha }}\ge \mathrm{50}$.

[Figure omitted. See PDF]

In order to evaluate the combined impact of pitch and roll, the tilted beam angle relative to the vertical, ${\mathit{\alpha }}_i$ for beam $i$, was calculated for each beam, following . The true pitch, ${\mathit{\varphi }}_{P_t}$, correcting for the influence of roll, is first calculated from the observed pitch and roll as A1$${\mathit{\varphi }}_{P_t}=\arctan \left(\tan \right({\mathit{\varphi }}_{\mathrm{P}}\left)\cos \right({\mathit{\varphi }}_{\mathrm{R}}\left)\right).$$ The tilted beam angle relative to the vertical, ${\mathit{\alpha }}_i$ for beam $i$, is then A2$$\begin{array}{rl}\cos \left({\mathit{\alpha }}_{\mathrm{1}}\right)& =-\sin \left({\mathit{\varphi }}_{\mathrm{R}}\right)\sin \left(\mathit{\theta }\right)+\cos \left(\mathit{\theta }\right)\sqrt{\mathrm{1}-{\sin }^{\mathrm{2}}\left({\mathit{\varphi }}_{\mathrm{R}}\right)-{\sin }^{\mathrm{2}}\left({\mathit{\varphi }}_{P_t}\right)}\\ \cos \left({\mathit{\alpha }}_{\mathrm{2}}\right)& =\sin \left({\mathit{\varphi }}_{\mathrm{R}}\right)\sin \left(\mathit{\theta }\right)+\cos \left(\mathit{\theta }\right)\sqrt{\mathrm{1}-{\sin }^{\mathrm{2}}\left({\mathit{\varphi }}_{\mathrm{R}}\right)-{\sin }^{\mathrm{2}}\left({\mathit{\varphi }}_{P_t}\right)}\\ \cos \left({\mathit{\alpha }}_{\mathrm{3}}\right)& =\sin \left({\mathit{\varphi }}_{P_t}\right)\sin \left(\mathit{\theta }\right)+\cos \left(\mathit{\theta }\right)\sqrt{\mathrm{1}-{\sin }^{\mathrm{2}}\left({\mathit{\varphi }}_{\mathrm{R}}\right)-{\sin }^{\mathrm{2}}\left({\mathit{\varphi }}_{P_t}\right)}\\ \cos \left({\mathit{\alpha }}_{\mathrm{4}}\right)& =-\sin \left({\mathit{\varphi }}_{P_t}\right)\sin \left(\mathit{\theta }\right)+\cos \left(\mathit{\theta }\right)\sqrt{\mathrm{1}-{\sin }^{\mathrm{2}}\left({\mathit{\varphi }}_{\mathrm{R}}\right)-{\sin }^{\mathrm{2}}\left({\mathit{\varphi }}_{P_t}\right)},\end{array}$$ where $\mathit{\theta }$ is the instrument beam angle of 20 or 30${}^{\circ }$ as appropriate and ${\mathit{\varphi }}_{P_t}=-{\mathit{\varphi }}_{P_t}$ if the instrument is downward-facing .

The variation in the ADCP beam average tilt for each of the instruments during each deployment is illustrated in Fig. . Panels (a) to (c) show the cumulative probability of $\mathrm{\Delta }\mathit{\alpha }$ for each instrument (column) and deployment (line colour), where $\mathrm{\Delta }\mathit{\alpha }$ is the mean across the four beams of the difference between the maximum and minimum ${\mathit{\alpha }}_i$ values for beam $i$ during a burst. Panels (d) to (f) show the cumulative probability of $n_{\mathit{\alpha }}$ for each instrument and deployment, where $n_{\mathit{\alpha }}$ is the mean across the four beams of $n_{{\mathit{\alpha }}_i}$, indicating the number of times that the sign of $a_i-⟨{\mathit{\alpha }}_i⟩$ changes from negative to positive during a burst.

There is a broadly consistent seasonal pattern in the distributions for all three instruments. The spring deployment periods 1 and 5 (blue and green lines, respectively) are similar, with $\mathrm{\Delta }\mathit{\alpha }$ typically increasing for the autumn deployment period 3 (yellow line), being the highest for the winter deployment period 4 (purple line), and being the lowest for the summer deployment period 2 (red line), which is consistent with the variation in wave energy conditions. The tables inset in each panel show the percentage of bursts for each deployment when the mean tilt range is $\ge \mathrm{5}$ and 10${}^{\circ }$, confirming that the tilt range for the upper and middle instruments is significantly more than for the lower instrument.

The distributions of $n_{\mathit{\alpha }}$ suggest that there is only limited variation between instruments and deployments. The middle and lower instruments exhibit a wider range of $n_{\mathit{\alpha }}$, although the median is $\sim \mathrm{30}$ oscillations per burst for all instruments and deployments.

Appendix B Synthesised along-beam velocity

The along-beam velocities observed by an ADCP, $b$, may include contributions due to the potentially sheared background flow, $\stackrel{\mathrm{‾}}{b}$, the orbital motion forced by surface gravity waves, $\stackrel{\mathrm{̃}}{b}$, and turbulent motions, $b^{\prime }$. We assume that these combine linearly as

B1$$b=\stackrel{\mathrm{‾}}{b}+\stackrel{\mathrm{̃}}{b}+b^{\prime }.$$ Along-beam velocity $b_{i,n}\left(t\right)$ for bin $n$ in beam $i$ at time $t$ is therefore synthesised by first determining the instantaneous ADCP bin position ${\mathit{x}}_{i,n}\left(t\right)=\left[x_{i,n}\right(t),y_{i,n}(t),z_{i,n}(t\left)\right]$. We then compute the Earth coordinate velocities at that location due to the background flow, ${\stackrel{\mathrm{‾}}{\mathbf{u}}}_{i,n}\left(t\right)=\left[{\stackrel{\mathrm{‾}}{u}}_{i,n}\right(t),{\stackrel{\mathrm{‾}}{v}}_{i,n}(t),{\stackrel{\mathrm{‾}}{w}}_{i,n}(t\left)\right]$, and surface waves, ${\stackrel{\mathrm{̃}}{\mathbf{u}}}_{i,n}\left(t\right)=\left[{\stackrel{\mathrm{̃}}{u}}_{i,n}\right(t),{\stackrel{\mathrm{̃}}{v}}_{i,n}(t),{\stackrel{\mathrm{̃}}{w}}_{i,n}(t\left)\right]$. Finally, we determine $b_{i,n}\left(t\right)$ as the along-beam component of ${\mathbf{u}}_{i,n}\left(t\right)={\stackrel{\mathrm{‾}}{\mathbf{u}}}_{i,n}\left(t\right)+{\stackrel{\mathrm{̃}}{\mathbf{u}}}_{i,n}\left(t\right)$ in the rotated beam coordinates and assuming that there is no turbulence such that $b^{\prime }$ is zero. Note that synthesised velocities are calculated directly from the specified background flow and any surface waves, without any allowance for observational noise or the spatial and temporal averaging that will affect actual observations to differing degrees depending on the operating mode.

All scenarios were based on a Teledyne RDI WorkHorse ADCP beam geometry, with a four-beam Janus-style convex transducer head such that with the instrument vertical, all beams have the same angle to the vertical, $\mathit{\theta }$ (${}^{\circ }$), with heading angle ${\mathit{\varphi }}_{\mathrm{H}}$ (${}^{\circ }$ N) indicating the compass direction of the horizontal projection of beam 3, pitch ${\mathit{\varphi }}_{\mathrm{P}}$ (${}^{\circ }$) indicating the rotation in the plane of beams 3 and 4, roll ${\mathit{\varphi }}_{\mathrm{R}}$ (${}^{\circ }$) indicating rotation in the plane of beams 1 and 2, and ${\mathit{\varphi }}_{\mathrm{P}}$ and ${\mathit{\varphi }}_{\mathrm{R}}$ at 0${}^{\circ }$ indicating that the ADCP is vertical with the convention for the direction of rotation as per , taking account of whether the ADCP is specified as upward- or downward-facing.

A standard burst configuration of 300 profiles collected at 1 Hz was adopted, with 30 bins per beam, a default vertical bin size of $\mathit{\delta }z=\mathrm{0.1}$ m, and bin 1 centred at $\mathit{\delta }{z}_{\mathrm{1}}=\mathrm{1.0}$ m.

B1 Bin positions

Bin positions were calculated in Cartesian coordinates relative to the ADCP transducer head, with the $x$ axis oriented due east, the $y$ axis due north, and the $z$ axis pointing vertically upward such that the transducer head is at $[x,y,z]=[\mathrm{0},\mathrm{0},\mathrm{0}]$.

Unit vectors describing the orientation of each beam when the ADCP is upward-facing and when ${\mathit{\varphi }}_H$, ${\mathit{\varphi }}_P$, and ${\mathit{\varphi }}_R$ are all 0${}^{\circ }$ are given by

B2$$\left[\begin{array}{cccc}{\widehat{\mathit{x}}}_{\mathbf{1}}& {\widehat{\mathit{x}}}_{\mathbf{2}}& {\widehat{\mathit{x}}}_{\mathbf{3}}& {\widehat{\mathit{x}}}_{\mathbf{4}}\end{array}\right]=\left[\begin{array}{cccc}\sin \mathit{\theta }& -\sin \mathit{\theta }& \mathrm{0}& \mathrm{0}\\ \mathrm{0}& \mathrm{0}& \sin \mathit{\theta }& -\sin \mathit{\theta }\\ \cos \mathit{\theta }& \cos \mathit{\theta }& \cos \mathit{\theta }& \cos \mathit{\theta }\end{array}\right],$$ and the along-beam bin centre position for all bins, common to all beams, is B3$$\mathbf{R}=(\mathit{\delta }{z}_{\mathrm{1}}+\mathit{\delta }z[\mathrm{0}\mathrm{1}\mathrm{2}\mathrm{\dots }N-\mathrm{1}\left]\right)/\cos \mathit{\theta },$$ where $N$ is the number of bins. The non-rotated coordinates for all of the bins in beam $i$ are then given by ${\mathit{x}}_{\mathit{i}}={\widehat{\mathit{x}}}_i\mathbf{R}$, as illustrated in panel (a) of Fig. .

Figure B1

Geometry for synthesis of along-beam velocities. (a) ${\mathbf{X}}_i$ coordinate positions for bin $n$ in each beam with instrument upright (${\mathit{\varphi }}_{\mathrm{P}}$ and ${\mathit{\varphi }}_{\mathrm{R}}$ both 0${}^{\circ }$) and heading angle ${\mathit{\varphi }}_{\mathrm{H}}=\mathrm{0}$${}^{\circ }$ N; (b) geometry for surface wave orbital velocity viewed from above with the block arrow showing the direction of wave propagation, $\mathit{\alpha }$ (${}^{\circ }$ N), the blue line being a wave front, and the grey arrows indicating ${\stackrel{\mathrm{̃}}{x}}_{i,n}\left(t\right)$, which is the distance from the wave front in the direction of wave propagation of beam $i$ bin $n$ at time $t$.

[Figure omitted. See PDF]

Heading variation was prescribed as a sinusoidal oscillation, with an initial angle, ${\mathit{\varphi }}_{\mathrm{H}}\left(\mathrm{0}\right)$ (${}^{\circ }$ N), an oscillation angular range, $\mathrm{\Delta }{\mathit{\varphi }}_{\mathrm{H}}$ (${}^{\circ }$), and a heading oscillation period, $t_{{\mathit{\varphi }}_{\mathrm{H}}}$ (s), such that at profile time $t$ B4$${\mathit{\varphi }}_{\mathrm{H}}\left(t\right)={\mathit{\varphi }}_{\mathrm{H}}\left(\mathrm{0}\right)+\left(\mathrm{\Delta }{\mathit{\varphi }}_{\mathrm{H}}/\mathrm{2}\right)\sin (\mathrm{2}\mathit{\pi }t/t_{{\mathit{\varphi }}_{\mathrm{H}}}),$$ with $t$ varying from 0 to 299 s over the burst and $\mathrm{\Delta }{\mathit{\varphi }}_{\mathrm{H}}=\mathrm{0}$${}^{\circ }$ or $t_{{\mathit{\varphi }}_{\mathrm{H}}}=\mathrm{0}$ s indicating a constant heading. Similarly, the pitch variation over the burst was defined as B5$${\mathit{\varphi }}_{\mathrm{P}}\left(t\right)={\mathit{\varphi }}_{\mathrm{P}}\left(\mathrm{0}\right)+\left(\mathrm{\Delta }{\mathit{\varphi }}_{\mathrm{P}}/\mathrm{2}\right)\sin (\mathrm{2}\mathit{\pi }t/t_{{\mathit{\varphi }}_{\mathrm{P}}})$$ and the roll variation as B6$${\mathit{\varphi }}_{\mathrm{R}}\left(t\right)={\mathit{\varphi }}_{\mathrm{R}}\left(\mathrm{0}\right)+\left(\mathrm{\Delta }{\mathit{\varphi }}_{\mathrm{R}}/\mathrm{2}\right)\sin \left(\mathrm{2}\mathit{\pi }\right(t+\mathit{\delta }{t}_{\mathrm{R}})/t_{{\mathit{\varphi }}_{\mathrm{R}}}),$$ with the only difference being the option to additionally specify $\mathit{\delta }{t}_{\mathrm{R}}$ as a phase offset.

Bin positions at time $t$ are then determined by rotation about the appropriate axes, with ${\mathit{\varphi }}_{\mathrm{H}}$ describing rotation about the $z$ axis, ${\mathit{\varphi }}_{\mathrm{P}}$ the $x$ axis, and ${\mathit{\varphi }}_{\mathrm{R}}$ the $y$ axis as follows. $$\begin{array}{cc}{\displaystyle }{\mathbf{M}}_{{\mathit{\varphi }}_{\mathrm{H}}}\left(t\right)& {\displaystyle }=\left[\begin{array}{ccc}\cos {\mathit{\varphi }}_{\mathrm{H}}\left(t\right)& \sin {\mathit{\varphi }}_{\mathrm{H}}\left(t\right)& \mathrm{0}\\ -\sin {\mathit{\varphi }}_{\mathrm{H}}\left(t\right)& \cos {\mathit{\varphi }}_{\mathrm{H}}\left(t\right)& \mathrm{0}\\ \mathrm{0}& \mathrm{0}& \mathrm{1}\end{array}\right]\\ {\displaystyle }{\mathbf{M}}_{{\mathit{\varphi }}_{\mathrm{P}}}\left(t\right)& {\displaystyle }=\left[\begin{array}{ccc}\mathrm{1}& \mathrm{0}& \mathrm{0}\\ \mathrm{0}& \cos {\mathit{\varphi }}_{\mathrm{P}}\left(t\right)& -\sin {\mathit{\varphi }}_{\mathrm{P}}\left(t\right)\\ \mathrm{0}& \sin {\mathit{\varphi }}_{\mathrm{P}}\left(t\right)& \cos {\mathit{\varphi }}_{\mathrm{P}}\left(t\right)\end{array}\right]\\ \text{B7}& {\displaystyle }{\mathbf{M}}_{{\mathit{\varphi }}_{\mathrm{R}}}\left(t\right)& {\displaystyle }=\left[\begin{array}{ccc}\cos {\mathit{\varphi }}_{\mathrm{R}}\left(t\right)& \mathrm{0}& \sin {\mathit{\varphi }}_{\mathrm{R}}\left(t\right)\\ \mathrm{0}& \mathrm{1}& \mathrm{0}\\ -\sin {\mathit{\varphi }}_{\mathrm{R}}\left(t\right)& \mathrm{0}& \cos {\mathit{\varphi }}_{\mathrm{R}}\left(t\right)\end{array}\right]\end{array}$$ This is subject only to ${\mathit{\varphi }}_{\mathrm{R}}={\mathit{\varphi }}_{\mathrm{R}}+\mathrm{180}$${}^{\circ }$ if the ADCP is specified as downward-facing. The positions for all bins in beam $i$ are then given by B8$${\mathit{x}}_i\left(t\right)=\left[\begin{array}{c}{x}_i\left(t\right)\\ y_i\left(t\right)\\ z_i\left(t\right)\end{array}\right]={\mathbf{M}}_{{\mathit{\varphi }}_{\mathrm{H}}}\left(t\right){\mathbf{M}}_{{\mathit{\varphi }}_{\mathrm{P}}}\left(t\right){\mathbf{M}}_{{\mathit{\varphi }}_{\mathrm{R}}}\left(t\right){\widehat{\mathit{X}}}_i\mathbf{R}.$$

B2 Velocity due to the background flow

A steady horizontal current, $\stackrel{\mathrm{‾}}{\mathit{u}}$, is defined with a speed at the transducer head depth, ${\stackrel{\mathrm{‾}}{u}}_{\mathrm{0}}$ (m s${}^{-\mathrm{1}}$), compass direction (to), $\mathit{\beta }$ (${}^{\circ }$ N), and vertical shear-squared, $S^{\mathrm{2}}$ (s${}^{-\mathrm{2}}$), with $S$ assumed to be positive such that current speed $\stackrel{\mathrm{‾}}{u}$ increases towards the surface and $S^{\mathrm{2}}=\mathrm{0}$ s${}^{-\mathrm{2}}$ indicating that the flow velocity is constant over the depth range.

The background flow velocity in Earth coordinates at the beam $i$ bin locations for time $t$ is then given by

B9$${\stackrel{\mathrm{‾}}{\mathit{u}}}_i\left(t\right)=\left[\begin{array}{c}{\stackrel{\mathrm{‾}}{u}}_i\left(t\right)\\ {\stackrel{\mathrm{‾}}{v}}_i\left(t\right)\\ {\stackrel{\mathrm{‾}}{w}}_i\left(t\right)\end{array}\right]=\left[\begin{array}{c}\sin \mathit{\beta }({\stackrel{\mathrm{‾}}{u}}_{\mathrm{0}}+S{z}_i(t\left)\right)\\ \cos \mathit{\beta }({\stackrel{\mathrm{‾}}{u}}_{\mathrm{0}}+S{z}_i(t\left)\right)\\ \mathrm{0}\end{array}\right],$$ with ${\stackrel{\mathrm{‾}}{u}}_i\left(t\right)$, ${\stackrel{\mathrm{‾}}{v}}_i\left(t\right)$, and ${\stackrel{\mathrm{‾}}{w}}_i\left(t\right)$ being the velocity components along the $x$, $y$, and $z$ axes, respectively.

B3 Orbital velocity due to surface waves

For a monochromatic surface gravity wave, linear wave theory describes the orbital motion as

B10$$\begin{array}{rl}u& ={\displaystyle \frac{gk}{\mathit{\omega }}}{A}_{\mathrm{0}}{\displaystyle \frac{\cosh \left(k\right(z+h\left)\right)}{\cosh \left(kh\right)}}\sin (kx-\mathit{\omega }t),\\ w& =-{\displaystyle \frac{gk}{\mathit{\omega }}}{A}_{\mathrm{0}}{\displaystyle \frac{\sinh \left(k\right(z+h\left)\right)}{\cosh \left(kh\right)}}\cos (kx-\mathit{\omega }t),\end{array}$$ where $u$ is the velocity component in the direction of wave propagation; $w$ is the vertical velocity component; $x$ is the distance in the direction of wave propagation; $z$ is depth referenced to the surface and positive upwards; $t$ is time; $g$ is acceleration due to gravity; $k$ is wavenumber given by $k=\mathrm{2}\mathit{\pi }/\mathit{\lambda }$, where $\mathit{\lambda }$ is the wavelength; $A_{\mathrm{0}}$ is the surface amplitude of the wave; and $\mathit{\omega }$ is the radian frequency given by $\mathit{\omega }=ck$, where $c$ is the wave phase speed from the wave dispersion equation: B11$$c^{\mathrm{2}}={\displaystyle \frac{{\mathit{\omega }}^{\mathrm{2}}}{k^{\mathrm{2}}}}={\displaystyle \frac{g}{k}}\tanh \left(kh\right),$$ with $h$ being the water column height such that $z=-h$ at the seabed .

From Eq. (), the wave orbital motion velocity in Earth coordinates at the beam $i$ bin locations for time $t$ is given by the following. B12$$\begin{array}{rl}{\stackrel{\mathrm{̃}}{\mathit{u}}}_i\left(t\right)& =\left[\begin{array}{c}{\stackrel{\mathrm{̃}}{U}}_i\left(t\right)\\ {\stackrel{\mathrm{̃}}{V}}_i\left(t\right)\\ {\stackrel{\mathrm{̃}}{W}}_i\left(t\right)\end{array}\right]\\ & =\left[\begin{array}{c}\sin \mathit{\alpha }\frac{gk}{\mathit{\omega }}{A}_{\mathrm{0}}\frac{\cosh \left(k\right({\stackrel{\mathrm{̃}}{z}}_i\left(t\right)+h\left)\right)}{\cosh \left(kh\right)}\sin \left(k{\stackrel{\mathrm{̃}}{x}}_i\right(t)-\mathit{\omega }t)\\ \cos \mathit{\alpha }\frac{gk}{\mathit{\omega }}{A}_{\mathrm{0}}\frac{\cosh \left(k\right({\stackrel{\mathrm{̃}}{z}}_i\left(t\right)+h\left)\right)}{\cosh \left(kh\right)}\sin \left(k{\stackrel{\mathrm{̃}}{x}}_i\right(t)-\mathit{\omega }t)\\ -\frac{gk}{\mathit{\omega }}{A}_{\mathrm{0}}\frac{\sinh \left(k\right({\stackrel{\mathrm{̃}}{z}}_i\left(t\right)+h\left)\right)}{\cosh \left(kh\right)}\cos \left(k{\stackrel{\mathrm{̃}}{x}}_i\right(t)-\mathit{\omega }t)\end{array}\right]\end{array}$$ Here, $\mathit{\alpha }$ (${}^{\circ }$ N) is the wave propagation compass direction (to), ${\stackrel{\mathrm{̃}}{z}}_i\left(t\right)=z_i\left(t\right)+z_{\mathrm{0}}$ is the beam $i$ bin depths referenced to the sea surface given an ADCP depth $z_{\mathrm{0}}$, and ${\stackrel{\mathrm{̃}}{x}}_i\left(t\right)$ is the array of rotated beam $i$ bin positions relative to the direction of wave propagation, calculated as B13$${\stackrel{\mathrm{̃}}{X}}_i=\left[\begin{array}{c}{x}_i\\ y_i\end{array}\right]\cdot \left[\begin{array}{c}\sin \mathit{\alpha }\\ \cos \mathit{\alpha }\end{array}\right],$$ which is the scalar dot product of the horizontal components of the rotated beam bin positions and the horizontal unit vector for the wave propagation direction, as illustrated in panel (b) of Fig. .

For scenarios including surface waves, the waves were specified in terms of their wavelength ($\mathit{\lambda }$; m), surface amplitude ($A_{\mathrm{0}}$; m), and compass direction of propagation (to – $\mathit{\alpha }$; ${}^{\circ }$ N). The depth of the ADCP, $z_{\mathrm{0}}$ (m), was specified within the range $-\mathrm{50}\mathrm{m}\le z_{\mathrm{0}}\le -\mathrm{20}\mathrm{m}$, and a standard water depth of $h=\mathrm{145}$ m was used for all scenarios.

B4 Along-beam velocity

The total velocity in Earth coordinates at the beam $i$ bin locations at time $t$ is then taken as the linear sum of the velocity due to the background flow and that due to surface waves as B14$${\mathit{u}}_i\left(t\right)={\stackrel{\mathrm{‾}}{\mathit{u}}}_i\left(t\right)+{\stackrel{\mathrm{̃}}{\mathit{u}}}_i\left(t\right).$$ The along-beam velocity for all of the bins in beam $i$, $b_i$, is then calculated as B15$$b_i=-{\mathit{u}}_{\mathit{i}}\cdot {\displaystyle \frac{{\mathit{x}}_{\mathit{i}}}{\left|{\mathit{x}}_i\right|}},$$ which is the scalar dot product projection of the total Earth coordinate velocity onto the rotated bin position vector ${\mathit{x}}_i$, with the negative sign included for consistency with the RDI convention that along-beam velocities are positive towards the transducer.

Data availability

The ADCP data referred to in Sect.  are currently being prepared for submission to the British Oceanographic Data Centre.

Author contributions

BDS undertook the analysis and prepared the paper. YDL and TPR commented on and contributed to the development of the paper.

Competing interests

The contact author has declared that neither they nor their co-authors have any competing interests.

Disclaimer

Publisher's note: Copernicus Publications remains neutral with regard to jurisdictional claims in published maps and institutional affiliations.

Acknowledgements

The observations described in Sect.  were collected as part of the United Kingdom (UK) Natural Environment Research Council (NERC) Carbon and Nutrient Dynamics and Fluxes over Shelf Systems (CaNDyFloSS) project, which forms part of the Shelf Sea Biogeochemistry research programme co-funded by the Department for Environment, Food and Rural Affairs (Defra). We thank Joanne E. Hopkins of the National Oceanography Centre, Liverpool, the crew of the RRS Discovery, and the National Marine Facilities staff for their assistance in collecting the ADCP observations, as well as Jon Turton at the Met Office for supplying the wave buoy data. Brian D. Scannell was supported through the Envision doctoral training programme and, subsequently, with Yueng-Djern Lenn by the PEANUTS project, part of the Changing Arctic Ocean programme funded by NERC and the German Federal Ministry of Education and Research. We also thank two anonymous reviewers for their detailed comments and suggestions, which have helped us to improve the paper.

Financial support

This research has been supported by the UK Research and Innovation (grant nos. NE/R01275X/1, NE/K00168X/1, and 1500369).

Review statement

This paper was edited by Erik van Sebille and reviewed by two anonymous referees.