OPEN
Light: Science & Applications (2017) 6, e16251; doi:http://dx.doi.org/10.1038/lsa.2016.251
Web End =10.1038/lsa.2016.251
Ofcial journal of the CIOMP 2047-7538/17
http://www.nature.com/lsa
Web End =www.nature.com/lsa
Hai-Long Zhou1,*, Dong-Zhi Fu2,*, Jian-Ji Dong1, Pei Zhang2, Dong-Xu Chen2, Xin-Lun Cai3, Fu-Li Li2 and Xin-Liang Zhang1
The ability to measure the orbital angular momentum (OAM) distribution of vortex light is essential for OAM applications. Although there have been many studies on the measurement of OAM modes, it is difcult to quantitatively and instantaneously measure the power distribution among different OAM modes, let alone measure the phase distribution among them. In this work, we propose an OAM complex spectrum analyzer that enables simultaneous measurements of the power and phase distributions of OAM modes by employing the rotational Doppler effect. The original OAM mode distribution is mapped to an electrical spectrum of beat signals using a photodetector. The power and phase distributions of superimposed OAM beams are successfully retrieved by analyzing the electrical spectrum. We also extend the measurement technique to other spatial modes, such as linear polarization modes. These results represent a new landmark in spatial mode analysis and show great potential for applications in OAM-based systems and optical communication systems with mode-division multiplexing.
Light: Science & Applications (2017) 6, e16251; doi:http://dx.doi.org/10.1038/lsa.2016.251
Web End =10.1038/lsa.2016.251; published online 21 April 2017
Keywords: mode analysis; orbital angular momentum; rotational Doppler effect
INTRODUCTION
Vortex light carries orbital angular momentum (OAM) characterized by exp(il), where is the angular coordinate and l is the topological charge (TC)1. OAM beams have been widely used in a variety of interesting applications, such as micromanipulation2,3, probing of the angular velocity of spinning microparticles or objects4,5, quantum information6,7 and optical communication8,9. Obviously, the TC is a basic physical parameter with which to characterize OAM light. The ability to distinguish different OAM modes is essential in an OAM-based optical system. Various interference methods have been developed to convert OAM modes into identiable intensity patterns, such as holographic detection with plasmonic photodiodes10 and the
generation of diffraction patterns using various apertures1115. In
these schemes, the superposition states of the OAM modes are difcult to distinguish. To distinguish these states, a common approach is to convert the unknown OAM modes into the fundamental mode (TC = 0) using a spatial light modulator (SLM) and then to calculate the power ratio of each mode after mode ltering1618. This approach requires the power of each OAM mode to be measured one by one or requires the use of multiple photodetectors, and thus, it is either time consuming or cumbersome. Another common approach is to sort the superposition states into different spatial locations, using methods such as a transformation from Cartesian to log-polar coordinates1922
or interferometric methods based on a rotation device2325. These
*These authors contributed equally to this work.
Received 27 June 2016; revised 31 October 2016; accepted 8 November 2016; accepted article preview online 11 November 2017
ORIGINAL ARTICLE
Orbital angular momentum complex spectrum analyzer for vortex light based on the rotational Doppler effect
techniques require photodetector arrays to detect the separated OAM states, and it is difcult to measure a large number of superposition states within a nite diffraction space. Some progress has also been made in measuring the power spectrum by mapping the OAM spectrum into the time domain2628, but the measured range and phase detection capabilities are limited. In light of the shortcomings of the state-of-the-art measurement techniques, it is desirable to develop an OAM complex spectrum analyzer that enables instantaneous and accurate measurements of the OAM mode distribution of light, similar to the function of an optical spectrum analyzer in characterizing a frequency distribution. An OAM complex spectrum analyzer is dened as a device that can simultaneously measure the power and phase distributions of OAM components. In 2014, the complex probability amplitudes of OAM states were successfully measured at the single-photon level through sequential weak and strong measurements29. However, OAM complex spectrum analyzers for use in classical information systems have received little attention and have yet to be achieved. In recent years, a novel transversal Doppler effect (rotational Doppler effect) associated with the transverse helical phase has been demonstrated, and Doppler velocimetry for rotating objects has been developed based on this effect30. This effect shows great potential for use in developing an OAM complex spectrum analyzer.
1Wuhan National Laboratory for Optoelectronics, School of Optical and Electronic Information, Huazhong University of Science and Technology, Wuhan 430074, China; 2Key
Laboratory for Quantum Information and Quantum Optoelectronic Devices, Shaanxi Province, Department of Applied Physics, Xian Jiaotong University, Xian 710049, China and
3State Key Laboratory of Optoelectronic Materials and Technologies and School of Physics and Engineering, Sun Yatsen University, Guangzhou 510275, China Correspondence: JJ Dong, Email: mailto:[email protected]
Web End [email protected] ; P Zhang, Email: mailto:[email protected]
Web End [email protected]
OAM complex spectrum analyzer
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In this article, we demonstrate a prototype of an OAM complex spectrum analyzer that employs the rotational Doppler effect. The system consists of unknown input OAM beams, a strong reference light, a spinning object, a mode lter and a photodetector. The original OAM mode distribution is mapped to an electrical spectrum of beat signals detected by the photodetector. The OAM power spectrum is measured with an inherent disturbance signal in the initial measurement. However, this disturbance signal can be fully eliminated via subtraction of the initial measurement from another constant-disturbance measurement. System calibration is also discussed, in which the input modes are mapped to beat signals with unequal efciencies; meanwhile, the phase distribution of the OAM modes can also be acquired via calibration. Similar to an optical spectrum analyzer, our scheme shows signicant potential for use in OAM complex spectral analysis and measurement for OAM-based systems and optical communication systems with mode-division multiplexing.
MATERIALS AND METHODSWhen OAM light illuminates a spinning object with a rotation speed of , as shown in Figure 1, the scattered light will exhibit a frequency shift that is related to the change in TC. The reduced Doppler shift is given by4
Df l mO=2p 1 where l is the TC of the incident light and m is the TC of the scattered light. To maintain the conservation of angular momentum, the spinning object should have a helical phase component of exp im ly
(ref. 31). Equation (1) suggests that the reduced
frequency shift depends on the TCs of the incident and scattered light and on the rotation speed. In other words, we can retrieve information regarding the OAM modes of the incident light by measuring the frequency shift of the scattered light at a certain rotation speed. This step is key to realizing an OAM complex spectrum analyzer. In our recent work31, we proposed a model to sufciently investigate the optical rotational Doppler effect based on a modal expansion method. Here, we present a simple derivation based on this model to explain how the effect can be used to measure the OAM complex spectrum. For simplicity, we ignore the difference along the radial direction; thus, the modulation function of the spinning object can be expressed in the form of a Fourier expansion as follows:
Mr; y XnAnexpinyexp inOt 2
where n is an integer index and t denotes the time. Assume that the input light consists of numerous unknown OAM modes expressed as
Ps1;2;?;N Bsexp i2pf texpilsy, whose TCs range from l1 to lN, where f is the frequency of the light and Bs is the complex amplitude of the corresponding mode. We introduce a reference light, expressed as gB0exp i2pf texpil0y, that illuminates the spinning object simul
taneously with the input light, where is a parameter that is used to tune the power of the reference light. The light scattered by the spinning object can be deduced as follows:
Eo
XmAZ
gB0exp i2pf tAm l0expimyexp im l0Ot
B1exp i2pf tAm l1expimyexp im l1Ot
B2exp i2pf tAm l2expimyexp im l2Ot
?
BNexp i2pf tAm lN expimyexp im lNOt
8 >
>
>
<
>
>
>
:
9 >
>
>
=
>
>
>
;
3
From Equation (3), we can see that all of the incident modes are converted by the spinning objects into a series of identical OAM modes that experience different Doppler frequency shifts, which vary linearly with respect to the TCs of the incident modes. After transmission over a certain distance, only one OAM mode (assume that this mode is OAMm; in general, it is OAM0) is selected via mode ltering and is then collected by a photodetector. Because of the beat effect, the collected temporal intensity can be derived as
Img
Ps1;2;?;N BsAm lsj j2 gB0Am l0j j2
2
P1rpoqrN BpAm lpBqAm lq
cos lp lqOt fp;q h i
2g
4
where fp;q angle BpAm lpB qA m lq
P1rprN BpAm lpB0Am l0
cos lp l0Ot fp;0 h i
. The collected intensity expressed in Equation (4) consists of three terms, namely, a direct current term, cross-beat signals among the input modes (called the disturbance signal in a real measurement), and beat signals between the input light and the reference light. If the power of the reference light is much greater than that of the input light, the disturbance signal can be ignored. Hence, the alternating current (AC) intensity can be approximately expressed as
Im;ACg 2P1rpoqrN BpAm lpBqAm lq
cos lp lqOt fp;q h i
2g
P1rprN BpAm lpB0Am l0
cos lp l0Ot fp;0 h i
E2g
P1rprN BpAm lpB0Am l0
cos lp l0Ot fp;0 h i
5
If lp l0p 1; 2; ?; N does not change in sign, then there is a
one-to-one mapping between the OAM modes and the frequencies; the coefcients are related to the corresponding complex amplitudes, and thus, a type of OAM mode analyzer can be designed. If all coefcients An and B0 are known, then the OAM complex spectrum can be obtained through spectral analysis. Note that fp;0 is a value
calculated by means of a complex integral when considering the difference along the radial direction and is not equal to the phase of the input OAM mode. Luckily, fp;0 always has a xed deviation relative to one of the input OAM modes, which can be calibrated by means of a pre-measurement; thus, the phase distribution of the input OAM modes can also be retrieved via system calibration.
In a real system, the disturbance signal will introduce some measurement errors regardless of its magnitude. In fact, the disturbance signal from the cross terms can be removed by changing the power of the reference light and then repeating the measurement. The subtraction of the AC signals in such a double measurement is
OAMm
Detection f =(l m)[afii9821]/2[afii9843]
[afii9821]
OAMl
x
z
Illumination
y
Figure 1 Schematic diagram of the rotational Doppler effect. When an OAM mode illuminates a spinning object, the scattered light experiences a frequency shift.
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Incident light
a b c
RDD
[afii9821]
Scattered light
Output signal
Input light
Reference light
OAM-1 OAM0 OAM1
OAM mode
A-t per mode
Time
OAM-4
OAM0
OAM4
OAM8
OAM-10
Amplitude Amplitude Amplitude Amplitude Amplitude
OAM-8
d
Time
Time
Time
Time
A-t per mode
A-t for all modes
Power spectrum
Amplitude Amplitude Amplitude Amplitude Amplitude
Amplitude
Relative power
Time
MF
Time
Time
Time
Time
Time
3
2
1
0 8 4 0 4 8 OAM mode
PD
Figure 2 Diagram of the OAM complex spectrum analyzer. (a) The incident light is composed of the input light and a reference light. Input light: the three-dimensional color images represent the spiral phase structures of the OAM modes, and the At curves present the dependency of the amplitude on time. Reference light: the reference light is chosen to be an OAM mode that lies outside the range of the input light. (b) Schematic representation of the OAM complex spectrum analyzer. The device consists of three components. A rotational Doppler device is used to realize Doppler shifts based on the rotational Doppler effect, and a mode lter is used to select OAM0. Hence, each mode is converted into OAM0 with a frequency shift that varies linearly with respect to the TC. Each input mode will beat with the strong reference mode, resulting in a beat signal, and the beat frequency will also vary linearly with respect to the TC. A photodetector is employed to measure the beat signals. (c) The scattered light is composed of numerous OAM modes. (d) The output signals are received by the photodetector. The rst column presents the beat signals between the reference mode and the various input modes. The beat frequency varies linearly with respect to the TC of the input mode, and the amplitude is proportional to that of the input mode. The total intensity is chaotic, but the power spectrum, which can be obtained through a Fourier transform of the total intensity collected by the photodetector, is consistent with the input OAM power spectrum. MF, mode lter; PD, photodetector; RDD, rotational Doppler device.
expressed as
ID Im;ACg2 Im;ACg
2g2 g
P1rprN BpAm lpB0Am l0
cos lp l0Ot fp;0 h i
6
Therefore, by performing a measurement using a strong reference light (called the initial measurement), we can measure the OAM power spectrum with an inherent disturbance signal. By then subtracting this initial measurement from another measurement obtained after changing the power of the reference light (called a constant-disturbance measurement), the inherent disturbance signal can be eliminated completely.
To evaluate the measurement accuracy, we dene the measurement error as
d
XNs1Bsj j2=
v !2
=N
XNq1Bq
2
Cs
j j2=
XNq1Cq
2
7
where Bsjs 1; 2; ?; N
f g are the theoretical OAM complex spectral
components and Csjs 1; 2; ?; N
f g are the experimental spectral
components.
Figure 2b shows a diagram of the proposed OAM complex spectrum analyzer, which consists of the input light to be measured, a strong reference light, a rotational Doppler device, a mode lter and a photodetector. The input light contains numerous unknown OAM modes within a certain nite-dimensional Hilbert space. For simplicity
of description, we assume that the TCs of the input OAM modes are within the range of 8 to 8, as shown in Figure 2a. We also introduce a strong coaxial reference light whose TC is outside the range of the TCs of the input OAM light. Here, we assume that the reference light is OAM-10 (TC = 10). When the input modes and the reference mode simultaneously illuminate a spinning object, the modes will experience different Doppler frequency shifts. The scattered light will thus contain many OAM modes, including the fundamental mode (OAM0) and other high-order modes, as illustrated in Figure 2c. The Doppler frequency shift is linear with respect to the input TC because only the fundamental mode is selected by the mode lter. The frequency differences will result in various beat signals, which are detected by the photodetector. The intensity of the reference light is much stronger than that of the input light; thus, the beat signals among the input modes can be ignored, and we need to consider only the beat signals between the input light and the reference light. As shown by the amplitudetime (At) curves presented in Figure 2d, OAM-8 and the reference mode OAM-10 will result in a beat signal at twice the speed of rotation. Similarly, the frequencies of the other beat signals will be proportional to the differences in TC between the input modes and the reference mode. Thus, the input OAM modes will be successfully mapped to the beat frequencies, and the amplitude of each beat signal will be proportional to that of the corresponding input OAM mode. Finally, we can obtain the OAM power spectrum through a Fourier transform of the total intensity collected by the photo-detector. We should note that because only OAM0 is collected by the
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photodetector, the overall efciency of this scheme is quite low. Even so, this drawback does not affect the measurement accuracy because a high-sensitivity photodetector can be used.
RESULTS AND DISCUSSIONExperimental setupWe designed a proof-of-principle experiment to demonstrate the proposed scheme. Figure 3 shows the experimental setup. The light emitted from a HeNe laser (wavelength of 633 nm) is expanded with two lenses (L1 and L2) and then illuminates SLM1. A half-wave plate and a polarization beam splitter are used to select the horizontal polarization to match the operating polarization of the SLM and to tune the input power. SLM1 is divided into three parts, as shown in the inset. The outer region is xed and is used to generate the input OAM modes to be measured, the middle region is used to introduce the reference light, and the innermost radius dening the inner region is adjusted to tune the power of the reference light. Only the input light (outer region) and the reference light (middle region) are diffracted to rst order by adding a grating in these two areas. The rst-order diffracted beam is selected using a pinhole (P1) and then illuminates the spinning object (SLM2). The pattern of SLM2 is rotated to scan the azimuth. Subsequently, the fundamental mode (OAM0) is selected by another pinhole (P2), and then a charge-coupled device (CCD) is used to determine the light intensity. Lenses (L3, L4 and L5) are employed to tune the optical path.
Measurement of OAM modesTo achieve well-proportioned mapping from the OAM modes to the electrical spectrum, the spinning object characterized by Equation (2) should have a uniform power distribution for each helical phase function. This effect can be implemented using a phase-only element with an iterative algorithm32,33. Here, an SLM (SLM2) is employed to
emulate the spinning object. Assume that the TCs of the input OAM modes are limited to a range of 8 to 8 and that the reference light is chosen to be OAM-10. In this case, for the spinning object, an even Fourier expansion of the modulation function ranging from 15 to 15 satises the requirement, as shown in Figure 4. The blue bars represent the ideal power weight of each helical phase component, and the red bars represent the theoretical results obtained using an iterative algorithm. We can see that an approximately even Fourier expansion ranging from 15 to 15 is achieved.
We rst measured several patterns of different OAM states. Figure 5a and 5b shows the simulated far-eld patterns and experimental results, respectively, for OAM-4, OAM-4 mixed with OAM6, OAM-4 mixed with OAM4 and a Gaussian distribution of OAM modes. The experimental patterns are consistent with the simulated results. In our
experiment, we set the OAM mode distribution of the input light to the same Gaussian distribution shown as the blue bars in Figure 5h. In the initial measurement, we ensured that the power of the reference light was higher than that of the input light by tuning the radius of the inner region of SLM1. The intensity determined by the CCD as a function of the rotation angle is shown in Figure 5c. We then calculated the power spectrum by means of a Fourier transform of the periodic signal collected by the CCD, as shown in Figure 5d. We can see that the measured OAM power spectrum is roughly consistent with the theoretical predictions but still exhibits signicant deviations, especially in the small-mode region. The measurement errors are 0.077 0.003 (corresponding to a range of 0.0740.080). The errors primarily arise from the neglected disturbance signal, namely, the cross terms in Equation (5). According to our theoretical model, this disturbance signal can be suppressed by increasing the power of the reference light. In a subsequent constant-disturbance measurement, we increased the power of the reference light by reducing the radius of the inner region of SLM1 to zero; the resulting received intensity and the corresponding power spectrum are shown in Figure 5e and 5f, respectively. The measurement errors are reduced to 0.037 0.001. It is clear that the deviations observed in this measurement are smaller, especially in the small-mode region. This nding demonstrates that the inherent disturbance signal from the cross terms in Equation (5) can indeed be ignored when the power of the reference light is much greater than the power of the input light. More importantly, in theory, the cross terms can be completely removed by subtracting the initial measurement from the constant-disturbance measurement, as shown in Equation (6). The measured power spectrum after intensity subtraction is shown in Figure 5g. As expected, the measurement errors are greatly decreased, to 0.017 0.002, and the deviations are strongly suppressed. The nal experimental results and the theoretical predictions of the mode distribution are presented in Figure 5h. One can see that the experimental results agree well with the theoretical predictions.
System calibration for a general spinning objectAlthough the measured power spectrum shows good consistency with the expected distribution, we still observe some deviations in Figure 5h, which primarily arise from unequal efciencies in the conversion of the input modes to beat signals. The characteristics of a spinning object are difcult to precisely determine in practice, and it is also difcult to determine the real phase distribution of the OAM modes without
0.03
Ideal
Sim
Normalized power
0.02
0.01
0 15 10 5 0 5
Order of harmonics (n)
10 15
Figure 4 Fourier harmonic distributions of the spinning object. The blue bars represent the ideal distribution, and the red bars represent the theoretical distribution obtained using an iterative algorithm. Sim, simulation.
SLM1
Laser
SLM2
HWP PBS
L1 L2
L3 L4
L5
P1
P2 CCD
Figure 3 Experimental setup for the measurement of an OAM complex spectrum. The light emitted from the laser illuminates SLM1 to generate the input light and the reference light, and the rst-order diffracted light is then selected using a pinhole (P1). Next, the light is directed onto a spinning object (SLM2), and OAM0 is selected from the scattered light using another pinhole (P2). Finally, a CCD is used to calculate the total light intensity of OAM0.
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system calibration; hence, an initial system calibration is required. Through system calibration, we can acquire the precise complex amplitude distribution (including both amplitude and phase) of the OAM modes. The calibration procedure is divided into three steps. First, we x the powers of the reference light and input light and then scan the input OAM modes to measure the complex amplitude of the beat signal between each input mode and the reference mode. The measured complex amplitudes are used as reference data for calibration. Second, we treat the input light as the light to be measured and measure the complex amplitudes of the harmonic signals according to Equations (5) or (6). Finally, the complex amplitude distribution of the input OAM modes is accurately retrieved by dividing the complex amplitudes of the harmonic signals by the reference data.
Now, we consider a more general case, in which the efciency of the conversion of each OAM mode to OAM0 is inconsistent or unknown; here, we must rst obtain the complex amplitude of the beat signal between each input OAM mode and the reference mode under the same conditions. Assume that the TCs of the input OAM modes are limited to a range of 10 to 10 and that the reference light is chosen to be OAM-15. First, we hold the power of the input light and reference light constant. Then, we scan the input OAM modes from OAM-10 to OAM10 to obtain the corresponding complex amplitudes of the beat signals. The amplitude and phase distributions of the beat signals between the input OAM modes and the reference mode are shown in Figure 6a and 6b, respectively. One can see that the complex amplitude distribution is complicated; this result arises because the modulation
function of the spinning object has a non-uniform harmonic distribution and the phase mapping is unclear. Here, the phase distribution in Figure 6b clearly shows the xed deviations between fp;0 and the phase distribution of the input OAM modes. After obtaining the complex amplitudes, we can begin to measure the OAM complex spectrum. To serve as an example, we designed a simple OAM mode superposition as the input light to be measured. The input modes consist of nite modes (TC = 10, 5, 0, 5, 10), whose initial intensities and phases are set to (1, 2, 1, 2, 1) and (, /2, 0, /2, ), respectively. The simulated and experimental patterns of the input light are presented in Figure 6c. Figure 6d and 6e shows the OAM power spectra measured without and with reference light, respectively, with measurement errors of0.077 0.002 and 0.068 0.002, respectively. The results in Figure 6d show the power spectrum of the inherent disturbance signal from the cross terms, and the results in Figure 6e display the OAM power spectrum with the same disturbance signal. Through the subtraction of double measurements, the deviations can be greatly suppressed, as shown in Figure 6f, and the measurement errors decrease to0.032 0.001. In this case, the errors are primarily due to uneven conversion efciencies and an unclear phase mapping. The results are then calibrated via normalization with respect to the reference data given in Figure 6a and 6b, and the measurement errors (0.006 0.001) become even smaller. The nal power and phase distributions of the OAM modes are presented in Figure 6g and 6h, respectively, and agree well with the theoretical calculations. In Figure 6h, the phases of the OAM modes with very low powers are set to null. Figure 7 demonstrates
a b
OAM 4
OAM 4,6 OAM 4,4 Input light OAM 4 OAM 4,6 OAM 4,4 Input light
Sim
Exp
c
e g
Relative intensity
1.4
1.3
1.2
Relative intensity
1.3
1.2
1.4 6 5 4 3 2 1 0
2 4 6 8 10 12 14
lp l0
l0= 10
16 18 20
Relative power
0 50 100 150 200 250 300 350
Rotation angle (degree)
0 50 100 150 200 250 300 350
Rotation angle (degree)
d f h
6 5 4 3 2 1 0
14
l0= 10
16 18 20
Sim
Exp
Relative power
Relative power
12
10
8
6
4
2
0
2 4 6 8 10 12 14
lp l0
l0= 10
Normalized power
0.25
0.2
0.15
0.1
0.05
0
2 4 6 8 10 12 14
lp l0
16 18 20 8 6 4 2 0 2 4 6
8
Topological charge
Figure 5 Experimental data for the measurement of a Gaussian distribution in the OAM basis. The (a) simulated patterns and (b) experimental results for OAM-4, OAM-4 mixed with OAM6, OAM-4 mixed with OAM4, and a Gaussian distribution of OAM modes. (c, d) The measured intensity over one period and the calculated OAM power spectrum obtained by introducing a reference light with TC = 10; in this case, the inherent disturbance signal from the neglected cross terms is obvious. (e, f) The results obtained after increasing the power of the reference light, which demonstrate that the cross terms can be suppressed by increasing the power of the reference light. (g) The OAM power spectrum obtained from a double measurement. The power spectrum for the double measurement has the lowest observed deviation. (h) The nal experimental results compared with the theoretical results. Exp, experiment; Sim, simulation.
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a
c
7
6
l0= 15
l0= 15
Relative amplitude Relative phase
5
4
3
2
1
3 2 1
1 2 3
0
0 10 5 0
Topological charge
Sim
Exp
5 10
b
10 5 0 5 10
Topological charge
d e f
2.5 12 10
8 6
Relative power
l0= 15 l0= 15 l0= 15
21.5
0.50 5 10 15 20 25
Relative power
Relative power
1
6543210 5 10 15 20 25
4 2 0
5 10 15 20 25
lp l0 lp l0 lp l0
g h
Sim
Exp
Sim
Exp
Normalized power
0.3
0.2
0.1
010 5 0 5 10 10 5 0 5 10
Topological charge Topological charge
Relative phase
3 2 1
1 2 3
0
Figure 6 Process of calibrating the OAM complex spectrum for a general spinning object. (a) The amplitude distribution and (b) the phase distribution of the beat signals between the input OAM modes and the reference mode. The data are acquired by measuring the individual complex amplitudes of the corresponding beat signals. (c) The simulated and experimental patterns of the input light. (d) The OAM power spectrum measured without a reference light. (e) The OAM power spectrum measured with a reference light. (f) The OAM power spectrum obtained from a double measurement. (g, h) The nal power and phase distributions of the OAM modes compared with the theoretical calculations. Exp, experiment; Sim, simulation.
a more general and complex measurement with calibration, where the unknown amplitude distribution is set to a triangular function and the phase is assumed to be irregular. The simulated and experimental patterns of the input light are presented in Figure 7a. The nal power and phase distributions of the OAM modes are presented in Figure 7b and 7c, respectively. The measurement errors are 0.005 0.001. We can see that the measured power distribution is well consistent with the theoretical calculations. Although there are some apparent errors in the phase measurement, this discrepancy is acceptable because the corresponding OAM modes are of very low power.
Notably, only one calibration is required for a xed spinning object, similar to the calibration of an optical spectrum analyzer. In some
cases, different spinning objects may be used to obtain different measurement accuracies or ranges. In such a case, the calibration must be repeated before mode measurements.
DiscussionIn the above, we presented an experimental design to demonstrate our proposed scheme at the proof-of-concept level. In this design, we use an SLM (SLM1) to simultaneously generate both the input light to be measured and the reference light. According to the theory of the rotational Doppler effect, the spinning object need not necessarily actually rotate. Equation (5) reveals that the rotation of an object is equivalent to the rotation of the surface modulation function of a xed
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a b c
0.16
Sim
Exp Sim
Exp
Sim
3
2
1
Exp
Normalized power
0.140.120.10.080.060.04
0.02010 5 0 5 10
Topological charge
Relative phase
0
1
2
3
10 5 0 5 10
Topological charge
Figure 7 Experimental data after calibration for a case in which the amplitude distribution of the input OAM modes is set to a triangular function. (a) Simulated and experimental patterns of the input light. The nal (b) power distribution and (c) phase distribution of the OAM modes compared with the theoretical calculations. Exp, experiment; Sim, simulation.
0.7
a b
3
Sim
Exp
Sim
Exp
0.60.50.40.30.2
0.10 2 1 0 1 2
Topological charge
Normalized power
Normalized power
Relative phase
2 1 0 1 2 3
2 1 0 1 2
Topological charge
0.70.60.50.40.30.2
0.10 LP21b LP11b LP01 LP11a LP21a
LP mode
c d
3 2 1 0 1 2 3
Sim
Exp
Sim
Exp
Relative phase
LP21b LP11b LP01 LP11a LP21a
LP mode
Figure 8 Experimental results in (a, b) the OAM basis and (c, d) the LP basis. The inset patterns show the intensity distributions of the corresponding modes. Exp, experiment; Sim, simulation.
object. Therefore, another SLM (SLM2) is employed to emulate a spinning object. We scan the azimuth by rotating the pattern implemented in SLM2 and record the collected intensity using a CCD. Because the frame rate of the SLM is approximately 60 Hz, a duration of a few seconds is required to complete the measurement. However, the use of a real spinning object would increase the requirements regarding the mechanical performance of the system or introduce mechanical vibrations, resulting in an unstable working state. In a real-world scenario, we can use a digital mirror device (DMD) instead of SLM2. A DMD has a function similar to that of an SLM but has a higher frame rate of up to 20 kHz, which is fast enough for practical applications. In addition, our conguration works only for a single wavelength. The same laser that generates the input light
can be used as the source of the reference light by modulating its output to create the reference mode. This approach is especially convenient in short-range applications. The source of the reference light can also be separated from that of the input light through mode ltering followed by amplication with built-in ampliers.
Our scheme can also be extended to measure the mode distribution in a few-mode ber by mapping the OAM modes to the eigenmodes of the ber. In most cases, only a small number of eigenmodes are used as independent channels, such as spatial modes (that is, LP01, LP11a, LP11b, LP21a and LP21b, where LP denotes a linear polarization mode and a and b represent the even and odd modes, respectively). These modes differ only in their azimuthal mode indices, similar to OAM modes. In fact, the OAM modes form an orthogonal basis for Fourier
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Light: Science & Applications
OAM complex spectrum analyzer
HL Zhou et al
8
expansion in the form of a complex exponential series, whereas the LP modes form an orthogonal basis for Fourier expansion in the form of a trigonometric series. It is possible to convert between these two bases. We rst measure the OAM complex spectrum and then map it to the complex spectrum based on the LP modes. The ability to measure the mode distribution in a ber has broad applications in optical ber communication with mode-division multiplexing.
Figure 8 presents a simple experimental demonstration of the ability to measure the LP mode distribution. The input light contains only two modes, LP01 and LP21a, which have the same power and a /2 phase difference. In our scheme, we rst measure the OAM complex spectrum, as shown in Figure 8a and 8b. These OAM modes are then expressed in the LP basis. The nal results presented in Figure 8c and 8d are accurate, demonstrating the ability to measure the LP modes. Note that the measured phases of LP21b, LP11b and LP11a can be revised to null because the corresponding amplitudes are null.
CONCLUSIONSIn summary, we demonstrate a prototype of an OAM complex spectrum analyzer based on the rotational Doppler effect. The system consists of unknown input OAM beams, a strong reference light beam, a spinning object, a mode lter and a photodetector. The OAM power spectrum is measured with an inherent disturbance signal via an initial measurement in the presence of a strong reference light. The disturbance signal arises from the cross terms of the input OAM modes and can be decreased by increasing the power ratio between the reference light and the input light. We further demonstrate that the disturbance signal can be eliminated by subtracting the initial measurement from a subsequent constant-disturbance measurement. Finally, we present an example in which we calibrate the OAM power spectrum for a general spinning surface, whose modulation function has an uneven distribution in the Fourier expansion along the azimuthal direction. Through calibration, the phase distribution can be determined. Similar to an optical spectrum analyzer, the proposed system offers the ability to measure the OAM complex spectrum of light, which has important applications in future OAM-based systems and optical communication systems with mode-division multiplexing.
CONFLICT OF INTERESTThe authors declare no conict of interest.
ACKNOWLEDGEMENTSThis work was partially supported by the National Basic Research Program of
China (Grant No. 2011CB301704), the Program for New Century Excellent
Talents of the Ministry of Education of China (Grant No. NCET-11-0168), the
Foundation for the Author of National Excellent Doctoral Dissertation of China
(Grant No. 201139), the National Natural Science Foundation of China (Grant
No. 11174096, 11374008, 11534008 and 61475052) and the Foundation for
Innovative Research Groups of the Natural Science Foundation of Hubei
Province (Grant No. 2014CFA004).
AUTHOR CONTRIBUTIONSHLZ and DZF contributed equally to this paper. HLZ proposed the study. HLZ,
DZF and DXC performed the experiment. PZ supervised the experiment. HLZ
and JJD analyzed the results and wrote the manuscript. JJD, PZ, FLL and XLZ
supervised the project and edited the manuscript. All authors discussed the
results and commented on the manuscript.
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Copyright Nature Publishing Group Apr 2017
Abstract
The ability to measure the orbital angular momentum (OAM) distribution of vortex light is essential for OAM applications. Although there have been many studies on the measurement of OAM modes, it is difcult to quantitatively and instantaneously measure the power distribution among different OAM modes, let alone measure the phase distribution among them. In this work, we propose an OAM complex spectrum analyzer that enables simultaneous measurements of the power and phase distributions of OAM modes by employing the rotational Doppler effect. The original OAM mode distribution is mapped to an electrical spectrum of beat signals using a photodetector. The power and phase distributions of superimposed OAM beams are successfully retrieved by analyzing the electrical spectrum. We also extend the measurement technique to other spatial modes, such as linear polarization modes. These results represent a new landmark in spatial mode analysis and show great potential for applications in OAM-based systems and optical communication systems with mode-division multiplexing.
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