Introduction
Soil losses caused by erosion are a major hazard in agricultural areas. Management of this risk requires a good understanding of various erosion forms and the quantification of eroded volumes over areas of several square kilometres, which is the scale of the elementary watershed as defined by . As noted by , topography is one of the major factors in most hazard analyses and the generation of DEMs plays a central role in their analysis. This is all the more true for gully erosion, considering that differencing DEMs theoretically allow for a direct estimation of eroded volumes. It is therefore appropriate to develop methods for generating detailed descriptions of landforms threatened by gully erosion at a limited cost. Cost-effective approaches are of great interest for monitoring on several spatial and temporal scales.
Before the advent of remotely piloted aircraft systems (RPASs), developments in remote sensing technology had already brought very high-resolution topographic data to the earth sciences community. Among these data, airborne lidar constituted a breakthrough, allowing for the characterisation of terrain surfaces with metre-size details. Such dense topographic data are of major importance for the description of hydrological-oriented geomorphological features . These even allowed for the development of the first algorithms for automatic gully detection. used a 2 m lidar DEM to detect gullies as zones with high curvature and low altitude relative to the average surrounding elevation computed within a moving window. With a lidar data set with a point density of 4 points m, performed curvature analyses to detect gully candidates in segments and then connect them to a complete network. Another example of curvature analysis is the work of , who identified gully headcuts from a 1 m lidar DEM as zones showing negative profile curvature below a given threshold and having a drainage area greater than 5000 m. proposed a method adapted to gullies of cushion peatlands using terrestrial lidar. In their work, gullies were delineated as polygons by detecting breaklines in the lidar DEM, and then artificial dams were manually positioned on the DEM, and finally, the formed sinks were filled. Occlusion effects due to the steep slopes of gully banks and the low-altitude point of view were noted by the authors. Most recently, used fuzzy logic on several topographic indices computed on a 1 m lidar DEM and combined it with image information and morphological operators to map gullies.
Although lidar technology has been developed for use aboard RPASs and has proven its potential in gully detection over large areas, this technology remains costly, which compromises its widespread use as an everyday monitoring tool. Structure from motion (SfM) and multi-view stereo (MVS) algorithms, which are recent developments in photogrammetry, represent new means of computing very high-resolution topographic data with a limited cost and have high potential in the geosciences as noted by and . In the specific field of gully erosion mapping and in line with lidar-based gully mapping approaches, proposed an automated algorithm tested on three DEMs of different types and scales – SfM MVS DEMs computed from ground and aerial images and a coarser and more classical DEM provided by the Spanish geographic institute – and demonstrated the potential of SfM MVS DEMs for gully erosion studies. For interested readers, in-depth details on SfM and MVS algorithms and their use in the geosciences can be found in the reviews of , , and .
The advent of SfM and MVS in the geosciences has made it possible to implement cost-effective solutions that can take advantage of developments previously achieved with lidar data for landform mapping applications. Indeed, SfM-based methods can be deployed with consumer-grade cameras and even smartphones (e.g. Micheletti 2015). As image data acquisition is now possible with fewer constraints, the field of 3-D modelling has opened to a wide range of applications from worldwide modelling of cities and landscapes to the geosciences (; ). In combination with small-format RPASs, the potential of SFM and MVS algorithms for 3-D mapping is huge, as reviewed by . However, covering several square kilometres with RPASs still requires costly fixed-wing or medium-format multi-rotor unmanned aircraft. Furthermore, the use of more affordable small-format rotary wing RPASs, which have shorter flight times, is limited in strong wind conditions. Finally, local regulations may hamper or even prohibit the use of autonomous aircraft in many places around the world. According to , this is the main restriction on the widespread use of these powerful and versatile technologies.
For all these reasons, kites, which were used for more than a century for aerial image acquisition, have been enjoying renewed interest for several years. In combination with most recent 3-D image processing algorithms, kites can hence be at the root of dependable and low-tech solutions, relying on the principles of so-called “frugal innovation”, which can simply be defined as “doing more with less” . In various fields in the geosciences, kites have indeed already been used with photogrammetric techniques for applications requiring 3-D mapping. used kite imagery to compute a 3-D model of an urban area. compared a DEM computed from kite aerial imagery to a ground survey and classified vegetation in mountainous areas with favourable results. also demonstrated the potential of kite aerial photography for DEM production over small areas (i.e. less than 1 ha) using off-the-shelf cameras and professional photogrammetry software. More recently, 3-D modelling from kite imagery was carried out by a small number of authors with SfM MVS software. have compared this technique (called “Ecosynth” by the authors) to lidar data for deriving elevation data and canopy-height models. performed centimetre 3-D mapping of vegetation in coastal areas and mapped coastal changes. assessed the accuracy of SfM MVS DEMs acquired with kites in comparison to lidar data in mountainous areas, where conditions limit the use of RPASs. More specifically, in the field of gully erosion, the potential of small-format cameras aboard kites and other platforms has been established by and , who realised the 3-D monitoring of several individual gullies in southern Spain.
Yet there are no studies at the headwater catchment scale – i.e. over areas of several square kilometres – showing the use of kites for 3-D topography acquisition and gully erosion mapping. Indeed, kites suffer from several limitations, of which flight control is the most challenging, as noted by . Some authors have given instructions for ensuring proper data acquisition with kites: used graduated lines to control flight altitude, and dedicated a chapter section to the principles and methods of kite aerial photography. However, the kite's ability to follow a predefined flight plan that enables 3-D coverage of several square kilometres has not yet been proven.
Thus, the aim of this study is to test the ability of low-tech kite aerial photography to obtain high-resolution DEMs that permit 3-D descriptions of active gullying in cultivated areas of several square kilometres. This goal jointly requires (i) the determination and assessment of the conditions that allow the use of a simple kite to acquire a suitable photogrammetric data set on a relatively large area and (ii) a 3-D map of gullies and assessment of the relevance of this map for erosion studies. To achieve this goal, we first expose and verify the conditions required to allow the use of a kite for photogrammetric acquisition over several square kilometres with numerical and field experiments. We then present a case study of image acquisition and processing on the Kamech catchment, located in northern Tunisia. Next, we propose a semi-automatic method for mapping gullies from the kite DEM. Finally we compared our results with independent ground surveys to assess the quality of the 3-D mapping of gullies and to exhibit the potential of kite DEMs with decimetre resolution and accuracy to study gully erosion.
Material and methods
Study site
The study site is the Kamech catchment, located in Cap Bon, a peninsula in north-eastern Tunisia (Fig. a).
Location of the Kamech test site and ground-truth data used in the SfM process. (a) Location of the Cap Bon peninsula, in north-eastern Tunisia; Kamech is marked in red. (b) Close-up of the Kamech catchment, 2.63 km, delineated in red; its outlet is an artificial lake, visible in the south-east of the catchment. (c) Close-up of the available ground-truth data around the lake; scale is given by the external graduations (projection UTM, EPSG : 32632); the dam is the linear feature visible on the south-eastern side of the lake. The ground-truth data set is composed of ground control points (GCPs, crosses), which are used to give spatial references to the image data set, and validation points (black dots), which are used to independently validate the DEM computed from the image data set.
[Figure omitted. See PDF]
Kamech is one of the two catchments of the OMERE long-term
hydro-meteorological research observatory (
Conditions for the use of a kite as a photogrammetric platform
To ensure photogrammetric image acquisition of several square kilometres, the method is based on the following hypothesis: with a very stable kite as a payload carrier, the position of the camera remains stationary relative to the kite operator. With this hypothesis, the flight path (i.e. the kite coordinates) is then a translation of the operator's course. Moreover, to use the simplest and most reliable apparatus, image acquisition is automatically triggered at a pre-set time interval. The flight plan can hence be prepared prior to the survey itself and followed on the ground without any need for remote control of the platform or a radio link between the camera and the operator. Thus, this hypothesis and the conditions ensuring its validity have to be carefully verified. This verification has been done with two complementary approaches, namely field observations and numerical simulations, which are described in the two following subsections.
Empirical kite flight characterisation
In this study, two delta kites were used, one with an area of 4 m and another with an area of 10 m. We used framed delta kites chosen from a large variety of kites because of their flight qualities (stability and high flight angles), easy assembly – with no need for adjustment in the field – and a reasonable payload capacity. A schematic representation and a close view of the equipment used for this study are shown in Fig. .
Left: schematic principle of kite image acquisition with a steady flight angle. Right: payload close-up, which consists of a tripod with (a) an automatic trigger (b) a camera and (c) a GPS logger. The yaw angle is the angle of the camera around the axis.
[Figure omitted. See PDF]
As shown, the camera was mounted under a protective tripod hanging from a long line forming a simple pendulum. This long pendulum smoothed out the potentially erratic movements of the kite. Finally, acting as a vane in the wind, the tripod allowed for natural aerodynamic stabilisation of the yaw angle, which is the rotation angle around the vertical axis of the tripod (Fig. c). The line used for all experimental set-ups was Cousin-Trestec TopLine Ultimate 16175, which is made of Dyneema®, a strong and light material. This line had a strength of 87 daN, a diameter of 0.8 mm and a linear mass density of 0.39 g m. The two delta kites performed a total of five flights, with wind conditions ranging from Beaufort 3 to Beaufort 7 and with line lengths ranging from 150 to 700 m. The use of the Beaufort scale was preferred in the field because it can be estimated from direct observation of land conditions (moving branches, raised dust, etc.) and does not require an anemometer. Camera and operator positions were simultaneously logged with a standalone QSTARZ BT1400S GPS data logger used with a 1 Hz acquisition rate (Fig. c). This data logger had a given accuracy of 3 m. These logs were used to compute effective kite flight angles from the pairs of camera and operator positions. Analysis of these flight angles was performed to verify the validity of our hypothesis and to empirically estimate the actual average flight angles. This information also made it possible to check the wind range in which the wing remained stable with a steady flight angle and with neither shocks nor sudden movements during the flight.
Simulations of kite flights
In addition to collecting the experimental data, numerical simulations of line shape and kite position were performed for different wind conditions (from 3 m s to 11 m s in increments of 2 m s) and for different line lengths (from 0 to 700 m). The materials used for kite lines are of particular interest. Highly resistant lines such as Dyneema® can be used in much smaller diameters than polyester of comparable strength, which results in less weight and aerodynamic drag. Polyester, Dyneema® and a perfect theoretical material with negligible mass and diameter were numerically compared to each other. For all the simulations, the rig load was 500 g, which is the actual mass of the rig we used (shown in Fig. ). Simulations were performed with the physical characteristics of the 10 m delta wing, which has a mass of 2.7 kg.
The model used was an ad hoc finite element model written in MATLAB. The line was sampled in sections of 1 m. The aerodynamics of the line were taken into account with the equation , where is the drag force in N, is the projected surface area in m, is the air bulk density in kg m, is the wind speed in m s, and is the dimensionless drag coefficient. This equation was also used to calculate the wind forces on the kite as a function of wind strength. All the parameters used for the simulations are reported in Table . These numerical simulations aimed to assess the impact of the kite line characteristics on the aforementioned hypothesis.
Parameters used for the simulation of line shapes and flight angle
| Parameter | Perfect line | Dyneema® | Polyester | 
|---|---|---|---|
| Line diameter (mm) | 0.01 | 0.8 | 2.5 | 
| Line linear mass density (g m) | 0.01 | 0.39 | 3 | 
| Resistance (daN) | n/a | 87 | 59 | 
| Pull angle () | 60 | ||
| Total mass (kg) | 2.7 (wing) 0.5 (payload) | ||
| Wing area (m) | 10 () | ||
| Wing drag | |||
| Line drag | (used for cylinders) | ||
| Air density (kg m) | |||
| Line length (m) | [0,700] | ||
| Wind speed (m s) | {3; 5; 7; 9; 11} | ||
Photogrammetric acquisition
Image acquisition was performed in September 2013 after the dry season, when vegetation cover was minimal. The equipment used for photogrammetric acquisition is shown in Fig. above. The Dyneema® kite line was graduated every 10 m for the first 100 m and then every 50 m with a simple colour/thickness coding system with a comparable approach to that used by . Image acquisition was performed with the 10 m kite. A maximum flight altitude of 500 m was chosen to acquire images with decimetre ground sampling distance. The corresponding line length was estimated with the worst case for the flying angle (50) and resulted in a maximum line length of 600 m. The targeted area was covered with parallel flight lines. These lines were oriented north-east to south-west along the global orientation of the catchment. The corresponding ground path was walked from the right bank towards the left bank. To simplify the field work, the operator remained at first on the same path near the right bank crest and unrolled different line lengths (150, 360 and then 600 m) so that the kite was positioned at the right downwind distance from the operator. Then, the operator continued to walk the rest of the ground path towards the right bank and covered the targeted area as planned. Images were taken with a Sony NEX-5N camera (Fig. b), which has a 16 Mpix 23.4 15.6 mm sensor. This camera was used with a fixed 18 mm focal length, and the image stabiliser was disabled, which are two important settings for the lens auto-calibration step in SfM processing. This camera was chosen as the best compromise at the time of the experiment between mass, suitability for photogrammetric analysis and cost (see Table in the Appendix). Automatic triggering was performed with a gentLED-Auto 05C intervalometer (Fig. a). A time interval of 5 s between each image was chosen to ensure sufficient overlap.
Complete coverage of the targeted area in the Kamech catchment was achieved within two flights of 3 h each. A total of 752 images were used to cover an area of 3.18 km. The maximum flight altitude of 500 m led to a maximum estimated ground pixel size of 0.13 m (see Table for a summary of all these data). The upstream part of the catchment being crossed by a power line, we avoided having the kite line near it for safety reasons. As a result, a small area of the catchment was not covered by multi-view imagery. However, more of the area downstream and outside the catchment was reached. As a result, the data set covered an area of 3.18 km, which exceeded the area of the catchment itself (2.63 km).
Flight conditions and characteristics of the photogrammetric survey.
| Estimated Beaufort | 4–5 | 
| Kite used | 10 m | 
| Line lengths (m) | 150, 360, 600 | 
| Flying heights (m) | 120, 300, 500 | 
| GCPs | 8 | 
| Focal length (mm) | 18 | 
| Sensor size (mm) | 23.4 15.6 | 
| Images used | 752 | 
| Max pixel size (m) | 0.13 | 
| Total covered surface (km) | 3.18 | 
Finally, eight points (cross marks on Fig. c) that were clearly visible in the kite images were used as GCPs. Their position was measured with a Topcon GR-3 RTK DGPS with a theoretical altimetric and planimetric accuracy of 1.5 cm. These GCPs were used as a spatial reference in the photogrammetric processing.
DEM computation
Kite images were processed with MicMac open-source software . This software implements both a bundle block adjustment and a hierarchical, true multi-view dense matching algorithm that is also used by the French Institut Géographique National to produce 3-D cartography. MicMac hierarchically computes multi-view dense matching from coarse grids to the full resolution by gradually refining the results at successive scales. The full resolution of the DEM is the average ground resolution of the images, which is estimated from the average flying height. This average flying height itself is estimated from the mean flight altitude and the average altitude of key points computed with the SIFT algorithm . All images covering the same point of interest are taken into account in the same bundle adjustment for the calculation of each point in the DEM. This procedure results in an altimetric precision of 1 pixel on average. The MicMac process is typical of SfM MVS algorithms (see Appendix) and is comparable with them (see for instance and ).
The SfM step (i.e. SIFT point recognition and matching plus bundle calibration) is completely automatic and followed by two manual steps. First, the area for dense image matching was selected. Second, the GCP positions were manually digitised in the images to give the project a cartographic reference. The automatic MVS dense image matching was finally run and resulted in a 0.20 m DEM. All image processing was performed on a laptop computer with an Intel Core i7-3840QM CPU at 2.80 GHz and 32 GB of RAM.
Gully detection
Similarly to , a gully is considered in this study to be a morphological object with a marked depression that is in the immediate proximity of a channel, the latter being determined by another algorithm. To delimit depressions, most recent studies use sliding windows. For example, use a sliding “normalised elevation” kernel. We chose another approach: we convolved the DEM with a Gaussian kernel by computing the inverse Fourier transform of the pointwise product of the Fourier transforms of the DEM and the Gaussian kernel. This method has two advantages. The first relates to computation time: with the Fourier transforms, the algorithm has a computational complexity of log()), with being the total number of pixels of the DEM. Sliding window algorithms have a computational complexity of , with being the window size in pixels. Hence, convolution with Fourier transforms is faster than filtering with sliding windows, except for very small windows. Above all, the processing time with convolution is independent of the kernel size. The second advantage is as follows: convolution by a Gaussian kernel simulates diffusive processes. Hence the DEM after convolution represents the hypothetical future shape of the ground surface after the processes involved in linear erosion have stopped and the processes leading to the healing of the gullies have begun.
For the delimitation of the channel network, the fully automated algorithm proposed by was tested at first (results not reported here). With this algorithm, the automated localisation of gully heads detected by high positive plan curvatures presented flaws. We observed that different threshold values – including the proposed default value – resulted either in an excessive number of missing gully heads or in categorising many anthropogenic depressions as gully heads, such as village streets or spaces between trees in orchards. As noted by , the automatic detection of channel heads is indeed most problematic for small-scale features such as some of those targeted by our work. Thus, gully heads were digitised from a shaded view of the DEM with the same type of expertise as one would use in the field. This approach was used by to produce their validation data set. The entire digitisation of the gully heads on the DEM was achieved within less than 2 h. Once the gully heads were digitised, the algorithm followed the flow chart in Fig. .
Flow chart of the method used to map gullies from the kite DEM. The letters associated with each step are referenced in the text describing the method in Sect.
[Figure omitted. See PDF]
The raw DEM (Fig. 3a) was convoluted with a Gaussian kernel (b) of a standard deviation of 10 m, which resulted in the smoothed DEM (c). We chose this value so that twice the standard deviation of the kernel was equal to the width of the largest gullies to be detected (i.e. 20 m). The raw DEM (a) was subtracted from the smoothed DEM (c) to create a depth map (d), which was therefore the estimated depth of the natural surface below the smoothed surface. Step (e) consisted of applying a threshold to the depth map and cleaning the result up. The threshold was chosen as slightly larger than the pixel size considering that lower differences in elevation would probably be noise. Features that did not show depths greater than 25 cm were hence discarded. The cleaning consisted of pruning out patches with volumes less than 1 m. This value allowed us to eliminate small-scale noise while keeping each detail of the gullies, even when they were made of discontinuous patches. Step (e) resulted in the (f) map. Steps (a) to (f) are illustrated with a section view in Fig. .
Principle of gully detection: (1) a Gaussian kernel with a 10 m standard deviation; (2) original (blue) and smoothed (red) topography; (3) raw negative differences between the original and smoothed topography; (4) detection of the potential gullies, then pruning out elements of less than 1 m; and (5) profiles of the detected gullies.
[Figure omitted. See PDF]
Steps (g) to (k) correspond to the extraction of the hydrological network. To map the hydrological network downstream of the previously digitised gully heads (g), a depression-free DEM (i) was generated from the raw DEM by filling gaps (h). The hydrological network (j) was generated by a steepest descent algorithm in (i) from gully heads (g). Considering the typical width of the gullies at the test site, a binary map (k) of the areas located less than 15 m from the network was computed. Intersecting the binary maps (f) and (k) resulted in the final gully map (m).
Validation
DEM quality
The kite DEM quality was evaluated on an independent validation data set composed of 469 points (see Fig. c for their localisation) and the median error, mean error and standard deviation of error were used as evaluation criteria. This control data set was surveyed with the same Topcon GR-3 RTK DGPS used for GCPs. These data came from a recurrent operation of bathymetry and topography of the reservoir performed a few weeks before image acquisition and from which points covered by vegetation were excluded. A qualitative assessment was also performed with a visual inspection of the kite DEM at full resolution.
Gully map
The quality of the gully map derived from the kite DEM was also assessed with independent data. The gully map was compared to a gully network derived from a field survey and completed by the interpretation of a QuickBird image. The field survey was carried out between 2009 and 2012 on nearly 70 % of the total gully and wadi network length of the Kamech catchment . Each gully and wadi was divided into sections whenever a branching (confluence) or significant change in the cross-section size was identified. For each gully upstream, middle and downstream positions were recorded with a handheld Garmin eTrex GPS. The precise delineation of each section was photo-interpreted on the orthorectified pan-sharpened QuickBird image using the upstream, middle and downstream GPS positions of the surveyed sections. Gully sections that were not described during the field survey were delineated on the orthorectified pan-sharpened QuickBird image only.
As in , the field-mapped network was considered as a reference and two parameters were computed from the match: “the false negative (underdetection), which is the length of the reference not included in the extracted network domain, and the false positive (overdetection), which is the length of the extracted network not included in the reference domain.” We also added a parameter that aimed to represent the overall accuracy and that was computed as the ratio of the total length of correctly mapped gullies to the total length of surveyed gullies.
Gully 3-D morphology
Finally, we tested the ability of the DEM to derive 3-D information that allows for gully morphology monitoring. This evaluation was based on a profile comparison of the kite DEM with a reference DEM derived from an intensive field topographic survey of a mid-size gully. This reference DEM was calculated on a 0.05 by 0.05 m grid from a very dense point data set acquired in 2009 using a total station that had an () accuracy better than 0.01 m . Standard statistics on the deviation between the kite DEM and the reference DEM were derived on an elevation profile of a path composed of a series of line segments.
Results
Simulated line characteristics
Figure shows the results of kite line shape simulations with different wind speeds, line characteristics and physical processes taken into account.
Comparison of the shapes on the 300 m lines (black bold) with perfect ones (thin grey) on a kite flown under different wind conditions and with different line materials. Simulations were performed at five wind speeds from 3 to 11 m s in steps of 2 m s. The load of the rig (Fig. – right) for the simulation is 500 g. Perfect lines (thin grey) were modelled with negligible weight and drag. (a) Dyneema® line (0.39 g m). (b) Polyester line (3 g m).
[Figure omitted. See PDF]
This figure revealed the following three findings: (i) with light and thin lines, the kite line is almost straight, and the flying angle is maximal; (ii) when the kite is flown in sufficiently strong wind, wind speed variations cause only small effective flight angle variations; and (iii) the latter observation is all the more true when the kite line is thin and light. These conclusions corroborate the field observations, which made us choose a thin and light line for photogrammetric acquisitions. Using a thin and light kite line – and a kite adapted to the actual wind conditions at the time of image acquisition – is hence a key condition for obtaining a steady flight angle and the required stable position of the kite relative to the operator.
Figure shows the simulated flight angle as a function of the line length for the Dyneema® line and polyester line.
Simulation of the variation in flight angle with the line length for different winds and line materials. Simulations were performed with five wind speeds from 3 to 11 m s in steps of 2 m s. (a) Dyneema® line. (b) Polyester line.
[Figure omitted. See PDF]
For both cases, the simulations showed that the flight angle dropped with increasing line length. The drop was slight for the Dyneema® but critical for the polyester line due to the stronger “banana shape” of the line observed in Fig. . Hence, the use of thin and light kite lines such as Dyneema® lines allows for kite flights with a steady flight angle at a given line length (Fig. ) but also with various line lengths (Fig. ). This steady flight angle makes the line length the only factor influencing the variation in the kite position relative to the operator. As a consequence, kite flights can effectively be planned and then properly realised. However, it is recommended to use a margin of security, considering the slight drop in flight angle for greatest line lengths. These findings were confirmed by the field experiments presented in the following section.
Observed kite flight angles
Figure shows the measured effective flight angles for the two kites used with the Dyneema® line for different line lengths and different wind conditions.
Observed flight angles for the two kites and various wind speed conditions and line lengths. Wind conditions (in italics) are expressed in the Beaufort scale. Measured flight angles were grouped in min/max boxes for each flight. Blue boxes represent the behaviour of the 10 m kite and black boxes represent the behaviour of the 4 m kite.
[Figure omitted. See PDF]
This figure corroborates the simulation results shown in Fig. : during field experiments, the flight angle dropped slightly but significantly with line length. This drop must hence be taken into account in preparation for image acquisition. We also noted that the smaller kite – which has a tail – flew at a significantly lower angle than the larger one. These experiments also included a flight (the leftmost blue box in Fig. ) with insufficient wind strength to fly the 10 m kite, which resulted in a wider range of flight angles and greater variability in the camera position relative to the operator. This result confirms that even with a thin and light line, the kite must fly within the appropriate wind conditions so that the flight angle remains steady.
DEM quality
The quantitative assessment of the DEM quality is reported in Table .
DEM altimetric error statistics.
| Mean (m) | 0.06 | 
| Median (m) | 0.07 | 
| Standard deviation (m) | 0.22 | 
| 90 % confidence interval (m) | [0.29; 0.81] | 
| Sample size | 469 | 
The error statistics demonstrated good agreement between the kite DEM and the independent DGPS-surveyed validation data set. In particular, the mean error and median error were smaller than the pixel size and the standard deviation of the error was of the order of the pixel size. These figures show that the DEM acquired by kite constitutes a reliable model of the catchment topography.
Moreover, a qualitative assessment of the kite DEM was carried out with a manual inspection of full-resolution DEM shaded views with three close-ups (Fig. ). The assessment showed that the kite DEM planimetric and altimetric resolutions allow for the visual detection of numerous landscape features, including most man-made structures (roads, tracks, buildings) and gully heads that were identified in the field (e.g. Fig. a and b). The plot locations and limits were also clearly depicted (Fig. a). Indeed, the boundaries between two separate adjacent plots are not exposed to tillage erosion and finally form small humps that are visible in the DEM. In the main thalweg (Fig. c), marks of regressive erosion were visible, and headcut locations could easily be identified. The potential of the kite DEM for use in extensive gully mapping within an area of several square kilometres is quantitatively evaluated in the next section.
Shaded images of the computed DEM over the Kamech test site. The main image is a classical shading of the DEM computed with a unique illumination source located in the east. The three zoomed-in panels are shaded images computed as the portion of visible sky at each point. This latter type of shading highlights local features such as steep slopes and areas of high curvature: (a) shows some cultivated plots with the plot borders easily visible and a gully head downstream of the plots; (b) shows a gully head; and (c) shows the main thalweg headcut, which is experiencing slow regressive erosion processes.
[Figure omitted. See PDF]
Assessment of 3-D gully modelling
An assessment of the gully network delineation was conducted at the scale of the whole channel network, and the 3-D restitution of the internal morphology of a gully was assessed at the scale of a single gully. Figure shows the final gully map obtained by the proposed method superimposed on the shaded DEM and a map of the validation results. Statistics of the comparison between the network extracted from the DEM and the field reference network are presented in Table .
Results of the gully mapping algorithm. (a) The gully network identified from the kite DEM is represented in red and superimposed on the shaded DEM. (b) Comparison with ground survey: yellow lines represent the part of the network correctly detected by our algorithm; black thick lines represent gullies detected by our algorithm where no gully was surveyed in the field (overdetection); blue lines represent gullies that were identified on the ground but not detected by our algorithm (underdetection); green lines represent gullies that were identified on ground but not used for error statistics, because they were outside the Kamech catchment area or their heads were outside of the area covered by the kite DEM.
[Figure omitted. See PDF]
Error statistics of the comparison at the scale of the channel network (Fig. ).
| Gully length | ||
|---|---|---|
| total (m) | relative | |
| Field reference | 18 237 | 100 % | 
| Good fit | 13 549 | 74 % | 
| False positives | 1513 | 8 % | 
| (Overdetection) | ||
| False negatives | 4688 | 26 % | 
| (Underdetection) | ||
The analysis of the gully map and the statistics showed a very good agreement between the detected gullies and the field reference. The overall accuracy was 74 %, with 8 % overdetection and 26 % of the network length unmapped. An inspection of the comparison map showed that most gullies that were not detected by our algorithm were located on the left bank (i.e. the south-eastern half), where gullies are less incised than those located on the right bank. Furthermore, most overdetections (gullies found by our algorithm but not surveyed on the ground) consisted of small gully segments mainly located on the right bank of the catchment.
Next, validation of the 3-D gully map was performed at the local scale and at very high resolution. Figure shows a 3-D comparison between a gully modelled by the kite DEM and dense measurements from a total station survey.
Comparison of the kite DEM with the ground survey. (a) Plan of the gully showing a gauging station at the gully outlet (white), two dense shrub patches of approximately 1 m height on the sides of the gully (dark black) and three patches of recent manure application (brown) in the field on the left bank of the gully; the graduated black line shows where profiles have been extracted. (b) Comparison of kite DEM (red) and ground survey (black) profiles; the vertical dashed lines delimit areas covered with shrubs. (c) Difference between the kite DEM and the ground survey along the same profile. Error statistics computed on this area are reported in Table .
[Figure omitted. See PDF]
Comparison of the profiles extracted from the kite DEM and from the surveyed DEM showed good agreement along the whole profile, except for areas covered by vegetation. The influence of vegetation was clearly detected (Fig. c), with elevation differences significantly differing from the surrounding noise. These observations were supported by the associated error statistics (Table ), with a mean error of 0.08 m, which decreases to 0.002 m when not taking into account zones covered by vegetation (parts of the profiles surrounded by vertical dashed lines in Fig. b and c). These results indicate that the kite DEM constitutes a reliable source of topographic data for the description of gully erosion forms. These findings seem likely to be extended for other gullies considering the good accordance between error statistics shown in Tables and .
Error statistics at the scale of the gully shown in Fig. .
| Error statistics (m) | Whole gully | Gully without vegetation | 
|---|---|---|
| Minimum | 0.49 | 0.49 | 
| 1st quartile | 0.13 | 0.14 | 
| Median | 0.003 | 0.01 | 
| Mean | 0.08 | 0.002 | 
| SD | 0.33 | 0.20 | 
| 3rd quartile | 0.19 | 0.14 | 
| Maximum | 1.52 | 0.66 | 
Moreover, a comparison of the quartiles estimated from the whole gully and from the non-vegetated part of the gully showed that vegetation mainly resulted in larger positive extrema, whereas the first, second and third quartiles remained comparable. The results at this scale were very similar to those computed with the 469 ground points sampled near the lake (Table above), with a standard deviation of the error for the DEM statistics being closer to that for the non-vegetated case. This result may indicate that vegetation is more likely to result in local errors rather than in a global deviation.
Discussion
In this study, we comprehensively assessed a cost-effective workflow to map gullies at the scale of the elementary watershed from images acquired by kite. Several important considerations have emerged. These considerations refer to the image acquisition step, the quality of the kite DEM and the accuracy of the gully map.
Large photogrammetric data sets with kites
Our study showed that achieving coverage of several square kilometres with
decimetre resolution and accuracy was possible with basic equipment for the
acquisition of a photogrammetric data set. These results represent an
improvement over those presented in , where the same
acquisition method was also used successfully over an area of only one-tenth
of that covered in this study. In other works that obtained DEMs with kites,
the maximum areas covered were also of the order of several hectares
(; ; ;
; ). Our results clearly
constitute an extension of the kite's capability. In particular, our work
presents novel findings on the conditions that must be met to make kite
photogrammetric acquisition successful at this scale. A correct realisation
of a planned flight is hence a critical issue for tethered platforms, as has
been noted by others (; ).
Numerical and field experiments have revealed that the choice of kite line
was a key factor in the success of our workflow. To the best of our
knowledge, the importance of the kite line for a proper photogrammetric
acquisition has rarely been considered with both numerical and field
experiments in previous works.  stressed out the
importance of a thin and light line on the basis of personal and external
If kites are proven to be valuable platforms for photogrammetric acquisition, they have some limitations. The two main limitations are (i) the fact that the line must be clear of obstacles and (ii) the need for a minimal wind speed. We faced the first issue in the most upstream part of the catchment because of a power line. Obstacles can also be found in densely vegetated or densely urbanised areas. Cases of obstruction have also been discussed by , who concluded that not every place is suitable for performing image acquisition from tethered platforms. The second issue, also noted by , can be approached as in , who used a kite to which a small helium blimp was added. used kites and balloons in alternation. In our opinion, in most cases, when the use of RPASs is not hampered by local regulations, kites associated with small-format multi-rotor RPASs represent a relevant all-weather solution. Indeed, the great advantage of small RPAS systems, in addition to being fairly inexpensive platforms, is the fact that they can provide very high-resolution spatio-temporal data with reduced response times in varied conditions . However, typical small-format RPASs may remain grounded during windy periods, thus preventing the requested rapid response. The other main niche for kites is related to local regulations, either for the flight itself or due to regulations regarding crossing borders with the equipment.
On another note, kites can fly for hours when weather conditions are appropriate. This autonomy represents a completely different paradigm to that for most RPASs. With the equipment presented above, the overall autonomy was only limited by the internal power supply of the camera. Within a single flight of 3 h, several thousand overlapping images can be acquired. This figure gives an idea of the mapping potential of this method, which produces DEMs in the gigapixel range.
DEM quality
Beyond the ability to acquire 3-D data over several square kilometres with kites, our aim was to demonstrate that these topographic data were reliable. We showed that the estimated altimetric bias was lower than the pixel size and that the estimated deviations were in the order of magnitude of pixel size. In other words, validation with an independent ground survey showed that the produced DEM had a decimetre resolution and accuracy.
Few works using kites have assessed the DEM elevation error. Our results compare quite well with these works. achieved a 0.13 m mean error, 0.36 m standard deviation of the error and 0.75 m maximal error on a 0.25 m resolution DEM (one thousand validation points). acquired images with an estimated 0.01–0.02 m ground sampling distance. The authors obtained a 0.01 m mean error and 0.065 m standard deviation error estimated with 399 independent validation points. acquired images with a 0.03–0.08 m ground sampling distance and computed a 0.04 m resolution DEM of a test site of roughly 10 ha. They estimated , and errors with 61 independent validation points and found a mean error of 0.04 m and RMSE of 0.16 m on the altitudes. computed a DEM with a ground sampling distance of 0.06 m. A quality check with 176 independent validation points resulted in a mean error of 0.04 m and a standard deviation of 0.07 m. Finally, with 0.004 m resolution images acquired on a 50 by 150 m area and a final DEM ground sampling distance of 0.05, estimated the mean error at 0.019 m and the standard deviation at 0.055 m with 86 validation points. Our work confirmed that the range of kites can be extended to several square kilometres with decimetre resolution while maintaining the accuracy in the pixel size range.
Gully network map and 3-D gully morphology
Although the overall accuracy of 74 % proved that our method was effective, the very process of validating the gully maps obtained from high-resolution DEM processing raises issues. To begin, validation methods are quite varied in the literature. Most authors (; ; ; ) have used manual digitisation of the gullies on the DEM as validation data and focused on different gully characteristics: width and depth , visual comparison (; ), and areal and volume difference (; ). Some authors (e.g. ) did not even validate the gully mapping results. Infrequently, studies such as have used field surveys as validation data for gullies that were automatically mapped from a DEM. Similarly to their study, our validation data were in the form of a channel network, and we used the same indicators as they did. We obtained a false positive rate (overdetection) of 8 % and a false negative rate (underdetection) of 26 %. Our results compare favourably to those of , who had false positive rates ranging from 5 to 16 % and false negative rates ranging from 29 to 55 %. Moreover, our results follow the same tendency, with false negatives rates being higher than false positives. This result may be explained by the fact that all gully mapping algorithms, including the one presented here, are based on the morphological characteristics of gullies (i.e. what a gully is) but do not benefit from characteristics that are known not to be shown by gullies (i.e. what a gully is not). In our opinion, this approach would be especially useful for avoiding confusion between gullies and man-made structures, which may be among the most delicate features to handle. This confusion may indeed explain some of the remaining inaccuracies we observed, and more generally, these issues have also been faced by others .
The detection of gullies in DEMs faces the difficulty of determining an unambiguous and generic definition of what a gully is. indicated that to their knowledge, no one has yet assessed where gullies “begin” in the transverse direction. Conversely, stated that “gully edges are the critical features for gully mapping”. noted that the assumptions usually used in channel-like extraction techniques do not apply to the environment of alluvial fans in which they propose an ad hoc gully mapping method. In brief, due to the variety of gully shapes and the fuzzy definition of their extent, each gully mapping algorithm in the literature so far requires the manual tuning of parameters and/or thresholds and is preferably applied to specific landscape types.
A possible workaround would be the use of multi-scale analysis, which was still seen by as a future research direction for high-resolution topography analysis. For future work in this direction, our algorithm has the advantage of being based on Fourier transforms instead of sliding windows, which makes the computation time independent of the characteristic size of the kernel and hence opens the door to multi-scale filtering with controlled computation times. Computing time is indeed one issue for DEM processing: for instance have been unable to process the full resolution of their largest DEM. Considering that upcoming topographic data sets will probably be more extensive and will have higher resolutions, this may still be an issue that will have to be mitigated by algorithmic improvements such as the one we have proposed.
The interest in multi-scale approaches is as strong as the 3-D information of such DEMs is rich, which is the case for the data obtained in our study. The comparison of dense elevation profiles between the kite DEM and ground reference hence showed good agreement. These findings thus confirmed, at a very local scale, the results on DEM accuracy found at the scale of the whole DEM. However, this detailed analysis raised the issue of vegetation cover. This issue is present in several classical cases where image-based approaches have limits that lidar does not have. However, with big image data sets, SfM MVS DEMs can reach densities that are comparable to or even exceed those of aerial lidar point clouds. This property would allow for the development of vegetation filtering algorithms tailored to these dense and multi-view image data. Second, our results can be compared to the work of , who used kites and balloons with a focus on two gullies. They determined that gully morphology and even gully changes could be assessed. In our case, with comparable sensibility and data available at the scale of the whole catchment, this morphological information would enable the description of different processes that occurred in different gullies or even at different times in the same gully, such as renewed erosion in older gully systems. Further work may then repeat our experiments to monitor ongoing gully erosion processes. These experiments would indeed be of great help, for instance, in understanding the source of the sediments responsible for reservoir siltation.
Conclusions
This paper proposes a complete workflow, from image acquisition with kites to a final gully map at the scale of a kilometre-square catchment with a careful assessment of each step. For image acquisition, we found that a key factor was the use of a thin and light line, which results in steady kite flight angles and thus a proper realisation of a kite photogrammetric flight in such large areas. Then, we showed that low-tech kite aerial photography could be successfully used for the acquisition of a high-resolution DEM covering more than three square kilometres with decimetre resolution and accuracy. Finally, we demonstrated that an appropriate gully mapping algorithm developed and applied to this DEM proved to be appropriate for the characterisation of gullies with 3-D decimetre details. Correct matches were obtained for 74 % of the gully lengths at the scale of an entire channel network. Still, kites require minimal wind speeds. This technique may therefore be thought of as a tool to be used in conjunction with small-format RPASs, especially when the latter cannot fly because of technical or administrative obstacles. Then, the proposed gully mapping method requires the intervention of an operator for the digitisation of gully heads. This approach may not be adapted to contexts with an excessive number of individual channels but proved appropriate in pruning the false positives produced by automatic procedures on anthropogenic features. Nevertheless, our study demonstrated that kite aerial photography using simple but appropriate equipment and an appropriate gully mapping algorithm represents a valuable tool for accurately surveying several hundred gullies at the scale of a kilometre-square watershed with decimetre detail, which may compare favourably with most ground surveys at these scales. These findings suggest that kites, SfM MVS, and adequate gully mapping algorithms provide greater access to high-resolution topographic data of kilometre-square watersheds and will facilitate a better understanding of gullying processes in a broader spectrum of conditions.
Image data and digital elevation model can be shared for collaboration purposes upon request by contacting the corresponding author.
MicMac workflow
Description of the commands used sequentially in the typical MicMac pipeline, from images to DEMs and orthophotographs:
- 
Tapioca: SIFT points are computed and matched; image resampling ratio affects the number of SIFT points.
 - 
Tapas: image orientation and auto-calibration takes place; memory requirements grow with the number of SIFT points and images and can be prohibitive; there are possible workarounds with RedTieP/OriRedTieP.
 - 
Tarama: a first raw mosaic of the area is computed; it can be used to obtain a quick estimate of the covered area.
 - 
SaisieMasq: the area of interest is manually delimited.
 - 
SaisieAppuis: GCP positions in images are manually measured.
 - 
GCPBascule: the model is georeferenced.
 - 
Malt: dense image matching occurs; the final DEM resampling ratio and regularisation parameters can be adjusted.
 - 
Tawny: orthophotograph mosaicking is completed.
 
Criteria for the choice of the camera
Advantages and drawbacks of three different camera technologies for acquisition with a kite for photogrammetry. The two first criteria are specific to kite-borne photogrammetry, while the last criteria are more general and apply to any photogrammetric application.
| Criteria | Importance | Compact | Hybrid | DSLR* | 
|---|---|---|---|---|
| Mass | high | |||
| Cost | medium | |||
| Prime lens | medium () | No | Yes | Yes | 
| Lens without moving parts | high | No | Yes | Yes | 
| Camera options() | high | |||
| Image quality | medium | 
Digital single-lens reflex camera. A lens with the zoom ring scotch-tapped on is a decent workaround if no prime lens is available. Includes the possibility of switching off the autofocus and the image stabiliser, both of which make auto-calibration difficult.
Notes for future kite users
It is worth noting that flying large kites, especially in strong winds, can raise security issues. Aside from and , this information is still barely reported in the scientific literature. The problems we faced appeared only under conditions of strong winds. These problems include small burns on hands, arms or clothes when the line is moving too fast or when the winder is temporarily out of control during a wind gust. This problem may also occur when the kite shows erratic movement in strongest winds when the operator is walking upwind. To avoid such problems, the following safety measures can be adopted: (i) ensuring physical protection of the operator with leather gloves, covering clothes and ensuring the safety of other people by keeping the downwind zone free of any lightweight and large equipment; (ii) keeping in mind that danger – and necessary expertise – grows with wind strength, a clever decision may be not to fly if conditions are not met; (iii) securing the flying gear (attaching it with hooks, for instance); and (iv) paying attention to equipment and people.
The authors declare no competing interests.
This article is part of the special issue “The use of remotely piloted aircraft systems (RPASs) in monitoring applications and management of natural hazards”. It is not associated with a conference.
Acknowledgements
The OMERE observatory (
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Abstract
Monitoring agricultural areas threatened by soil erosion often requires decimetre topographic information over areas of several square kilometres. Airborne lidar and remotely piloted aircraft system (RPAS) imagery have the ability to provide repeated decimetre-resolution and -accuracy digital elevation models (DEMs) covering these extents, which is unrealistic with ground surveys. However, various factors hamper the dissemination of these technologies in a wide range of situations, including local regulations for RPAS and the cost for airborne laser systems and medium-format RPAS imagery. The goal of this study is to investigate the ability of low-tech kite aerial photography to obtain DEMs with decimetre resolution and accuracy that permit 3-D descriptions of active gullying in cultivated areas of several square kilometres. To this end, we developed and assessed a two-step workflow. First, we used both heuristic experimental approaches in field and numerical simulations to determine the conditions that make a photogrammetric flight possible and effective over several square kilometres with a kite and a consumer-grade camera. Second, we mapped and characterised the entire gully system of a test catchment in 3-D. We showed numerically and experimentally that using a thin and light line for the kite is key for a complete 3-D coverage over several square kilometres. We thus obtained a decimetre-resolution DEM covering 3.18 km
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Details
1 LISAH, Univ Montpellier, INRA, IRD, Montpellier SupAgro, Montpellier, France
2 El Manar University, National Engineering School of Tunis, LTSIRS, B.P 37, 1002 Tunis-Belvédère, Tunis, Tunisia
3 Rural Engineering Laboratory, National Research Institute of Rural Engineering, Water and Forests, INRGREF, Rue Hédi Karray El Menzah IV – B.P 10, Ariana 2080, Tunisia
4 Université Paris-Est, IGN/SR, LOEMI, 73 avenue de Paris, 94165 Saint-Mandé, France





