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Fig. 1 shows a schematic of the proposed DNRDE detection scheme for determining the orientation of the rotating axis. We first created a synthetic OAM light field that satisfies the orthogonality and rotational symmetry requirements by exploiting the coherent superposition of specific conjugate-superposed OAM light fields. The synthetic OAM light field was further guided vertically onto the surface of a rotating object with a misaligned rotating shaft O′ relative to optical axis O. Subsequently, the incident tailored light field was scattered from the rough surface of the rotating object. Backscattered light experienced noncoaxial rotational Doppler shifts (RDSs). The orientation of the rotating axis can be unambiguously ascertained in real time by detecting arbitrary dual-point Doppler shifts within two illuminated local scatterers and comparing the magnitudes of these two shifts using a prescribed frequency threshold. Mathematically, synthetic OAM light fields can be produced by the superposition of N (> 1) pairs of conjugate superposed OAM light fields with OAM indices of ln = 4n or ln = 2n+1 (details in the Supplementary Information (SI)), which are formulated in the cylindrical coordinates (r, φ, z) at z = 0 as
Fig. 1 Diagram of dual-point noncoaxial RDE of customized OAM light fields for rotating-axis detection. The customized OAM light field with four hotspots satisfying the orthogonality and rotational symmetry, is normally directed onto the rough rotating surface with the rotating axis being misaligned with the optical axis optical axis. Two points, P1 and P2, located within the hotspots on the rotating surface were selected. These points experienced distinct RDSs, which are sensitive to the rotating axis orientations. By detecting the two noncoaxial RDSs in the back-scattered light signals, the rotating axis orientations can be unambiguously determined. Here, P1, P2, P3, and P4 are four local scatterers illuminated within four hotspots; Ω represents the rotating velocity; O and O′ are the beam center of the customized OAM light field and the rotating center of the object, respectively; $ \overrightarrow{r} $ and $ \overrightarrow{R} $ are the beam and rotating radii of local scatters; $ \overrightarrow{S} $ is the Poynting vector; and $ {\overrightarrow{v}_{{}_{1}} }$ is the linear velocity at point P1. β is the skew angle of the Poynting vector and optical axis direction.
$$ {E_N}\left( {r,\varphi } \right){\kern 1pt} {\kern 1pt} = {\kern 1pt} {\kern 1pt} \sum\limits_{n = 1}^N E \left( r \right)\left[ {\exp \left( {i{l_n}\varphi } \right) + \exp \left( { - i{l_n}\varphi } \right)} \right] $$ (1) where E(r) denotes the r-dependent complex amplitude and N denotes the total pair number of coherently superimposed phase-conjugated OAM light fields.
To illustrate our detection scheme, we select E2 as a representative example, but other synthetic OAM light fields that satisfy Eq. 1 can also be used for this purpose. Fig. 2a–c depict the conjugate superposed OAM light fields E0,±ln with OAM indices of l1, l2 as well as the corresponding synthetic OAM light field distributions with N = 2, respectively. Fig. 2a, b shows that the phase-conjugate superposed OAM light fields exhibit petal-shaped patterns, while in Fig. 2c, four hotspots with orthogonality and rotational symmetry emerge accompanying by tiny sidelobes between the two adjacent hot ones. We also assessed the maximum intensity of the sidelobes relative to the main lobes by scanning the synthetic OAM light field along the x-axis and the line y = 0.8ω0, as shown in Fig. 2d. The results indicate that the maximum intensity of the sidelobes is < 33%, which would have almost no impact on our detection processes when the echo signals are collected by using the single-mode fibers or optical modal filters.
Fig. 2 Concept of the synthetic OAM light field and principle of DNRDE for detecting rotating axis orientations. a and b Light field distributions of two conjugate-superposed OAM light fields with OAM indices l1 = 4 and l2 = 8, respectively. c The synthetic OAM light field and d intensity profiles of this customized OAM light field along the x-axis and the line y = 0.8ω0 for ascertaining the maximum intensity of sidelobes relative to main lobes. e Principle of DNRDE. f Principle for the real-time detection of rotating axis orientations by exploiting the comparison of the relative magnitudes of dual-point noncoaxial RDSs fRDS-1 at P1 (light blue solid line) and fRDS-2 at P2 (brown solid line) with a frequency threshold fth = 763.9 Hz (circular green dotted line) that is determined by the magnitudes of these two OAM-associated shifts together with the quadrant boundaries. Additionally, the polar axis in the polar coordinates denotes the dual-point noncoaxial RDS values, (unit: kHz) and the polar angle represents the rotating axis orientation. All findings were obtained using the following simulated parameters: λ = 532 nm, c = 3 × 108 m/s, ω0 = 1 mm.
When guiding such a well-established OAM light field onto a rotating rough surface with angular velocity Ω in a noncoaxial manner, the illuminated local scatters on the rotating surface would induce RDSs. We arbitrarily selected two local scatterers on this surface, P1 and P2, that were illuminated by the two hotspots. By simultaneously detecting these two echo light signals, we could determine the DNRDE. By comparing the magnitudes of the dual-point non-coaxial RDSs with a certain frequency threshold determined by these two shifts and quadrant boundaries, the rotating axis can be unambiguously ascertained with only a one-shot measurement. According to the mathematical deviations in Supplementary Note 2, the dual-point noncoaxial RDSs of the customised OAM light field at these two points can be expressed as follows:
$$ {f_{RDE - 1}} = \frac{{\left| {{l_n}} \right|\Omega \left( {r - d\cos \gamma } \right)}}{{\pi r}} $$ (2) $$ {f_{RDE - 2}} = \frac{{\left| {{l_n}} \right|\Omega \left( {r - d\sin \gamma } \right)}}{{\pi r}} $$ (3) Here, $d$ denotes the distance between the rotary and optical axes and $\gamma $ represents the rotating axis orientations. Using Eqs. 2, 3, the orientations of the rotating axes can be determined by measuring the RDSs once the rotating velocity, light beam radius, and axis distance between the optical axis and rotating shaft are known in advance. To demonstrate this, we simulated the dependence of the rotating axis orientations on the DNRDE shown in Fig. 2f, with a preset rotating velocity Ω = 300 rad/s, OAM index l2 = 8, synthetic OAM light field radius r = 2.5 mm, and axis distance d = 5 mm, which match our upcoming experimental conditions. As shown in Fig. 2f, we first compared a single-point non-coaxial RDS, such as fRDS-1 at point P1 (light blue solid line), with the frequency threshold. This shift is obviously less than the frequency threshold fth for the rotating axes in the first and fourth ( I and IV) quadrants, whereas it is greater than fth for those in the second and third (II and III) quadrants, where fth = 763.9 Hz (illustrated with circular green dotted lines in Fig. 2f) is the frequency threshold determined by the magnitudes of these two shifts with the quadrant boundaries (Fig. 2f). Obviously, in this case, a single-point noncoaxial RDS fails to distinguish the rotating axis orientations through one-shot measurements because the single-point frequency shift fRDS-1 in quadrants Ⅰ- and Ⅳ and quadrantsⅡ- and Ⅲ possess the same magnitude rule versus the frequency threshold fth, respectively. To overcome this limitation, we examined the dual-point frequency shifts (fRDS-1 and fRDS-2 at P1 and P2, respectively) and compared them with fth, as depicted in Fig. 2f. Consequently, we discovered that for the rotating axes in each of the quadrants: in quadrant I, fRDS-1, fRDS-2 < fth; in quadrant II-, fRDS-1 > fth, fRDS-2 < fth; in quadrant III, fRDS-1, fRDS-2 > fth; and in quadrant IV, fRDS-1 < fth, fRDS-2 > fth. Therefore, the rotating axis orientations can be discriminated in real time by comparing the magnitudes of the detected dual-point noncoaxial RDSs with the prescribed frequency threshold. Any two local scatterers illuminated within the four hotspots can be selected to detect the noncoaxial RDE and determine the rotating axis orientations.
Furthermore, Fig. 2f shows that the rotating axis in quadrant III elicits significantly larger dual-point non-coaxial RDSs at points P1 and P2, compared to the other quadrants (i.e. the measured points P1 and P2 are lie within positive x- and y-axes, respectively, whereas the simultaneous maxima of fRDS-1 and fRDS-2 versus fth fall into quadrant III). This observation suggests that dual-point noncoaxial RDSs are more sensitive to the presence of oppositely oriented rotating axes. Exploiting these larger shifts can facilitate the highly sensitive and accurate detection of the rotating axes in specific quadrants. Therefore, we further investigate the other dual points in Fig. 4 and find that this phenomenon is consistent across the three pairs of adjacent dual points, namely points 1 and 4, points 2 and 3, and points 3 and 4. By detecting the Doppler shifts at these four particular dual points, full orientations of the rotating axis can be determined with higher sensitivity and thus higher accuracy because the enlarged dual-point noncoaxial RDSs move away from the low-frequency noise domain, leading to a salient signal-to-noise ratio.
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In the proof-of-concept experiment, as shown in Fig. S2, we generated a high-quality synthetic OAM light field E2 using a spatial light modulator with an incorporated 4f system to detect the rotating axis in real time (Methods and Supplementary Notes 3 and 4). To validate the rotating axis orientations, we initially varied the rotating axis orientations to detect the dual-point noncoaxial RDSs in four quadrants (i.e., Ⅰ-, Ⅱ-, Ⅲ-, and Ⅳ) respectively. The axis distance from the optical axis was fixed at 5 mm, while the rotating velocity was set to a pre-determined value of 300 rad/s. The outcomes of the measurements are separately depicted in Fig. 3a–d, where the four individual Doppler signal peaks are detected in the power spectra for each of the measured points. This happened because in addition to the ±4th- and ±8th-order OAM modes, the rotating surface induced RDSs in their interferometric modes (i.e., −4th and +8th or +4th and −8th orders and −4th and −8th or +4th and +8th orders). This experimental finding is in a good agreement that from a previous study2. Even after undergoing digital signal post-processing, which introduces strong noise, the signal distribution law is still preserved in the low-frequency domain. Fig. 3a shows that the measured noncoaxial RDSs at points P1 and P2 for ±8th-order OAM modes were all below the frequency threshold fth. fth relates to the OAM index that determines the dual-point noncoaxial RDSs, and here it corresponds to the ±8th-order OAM modes. Thus, it is necessary to carefully distinguish the dual-point Doppler signal peaks at matched OAM modes to perform peer-to-peer comparisons. In Fig. 3b, the measured noncoaxial RDSs at points P1 and P2 are 1778.4 Hz (> fth) and 380.14 Hz (< fth), respectively. Fig. 3c shows that when the axis orientation is prior-settled in quadrant Ⅲ, i.e., southwest orientation, the measured frequency shifts at points P1 and P2 are both > fth. In a similar way, in Fig. 3d, the measured noncoaxial RDSs at points P1 and P2 are 471.17 Hz (< fth) and 1669.66 Hz (> fth), respectively. The measured outcomes validate our theoretical analyses. For more complicated emitted light fields EN with N ≥ 3, the Doppler peaks in the measured Doppler spectra multiply. At this point, it becomes difficult to distinguish the Doppler peak corresponding to the prescribed OAM components, thus, leading to an unclear discrimination of the rotating axis orientations. To cope with this issue, we propose a general strategy that uses optical modal filters to sort out specific modal components within scattered light, enabling the detection of only a single Doppler signal peak (the following context). Hence, by comparing the measured dual-point noncoaxial RDSs towards the synthetic OAM light field with the prescribed frequency threshold, the rotating axis orientations can be unambiguously determined.
Fig. 3 Measured power spectra as the function of the noncoaxial RDSs at the two points P1 and P2, exploited to determine rotating axis orientations. Dual-point noncoaxial RDSs when the rotating axes are prior-settled in the a I-quadrant; b II-quadrant; c III-quadrant; d IV-quadrant, respectively. The azury and red arrows corresponding to points P1 and P2, respectively, refer to the Doppler signal peaks of ±8-order OAM modes. The frequency threshold fth = 763.9 Hz (green dotted line).
To further validate our metrological principle for probing rotating axis orientations, we measured distinct dual-point non-coaxial RDSs at points P1 and P3, P1 and P4, P2 and P3, and P3 and P4. As illustrated in Fig. 4, the measured outcomes matched the theoretical predictions well, demonstrating the efficacy of our method in discriminating rotating axis orientations using arbitrarily selected dual points in our engineered light field. Furthermore, Fig. 4a shows that the rotating axes in quadrants II and III are much more sensitive to the Doppler shifts of point 1, whereas point 3 responds more easily to the rotating axes in quadrants I and IV. An identical law is also applicable to the other dual points P2 and P4 (not shown here). In other words, symmetrical dual points (including only P1 and P3, as well as P2 and P4) can be employed to measure axis orientations in real time by comparing their magnitudes with fth, but in these two cases, the rotating axis fails to be saliently sensible to dual points simultaneously (i.e. ${f_{RDE - 1}}$ and ${f_{RDE - 3}}$ cannot be simultaneously larger than fth; the same applies to ${f_{RDE - 2}}$ and ${f_{RDE - 4}}$). In contrast, the measured results illustrated in Fig. 4b–d show that the rotating axial orientations are more sensitive to oppositely oriented dual-point noncoaxial RDSs. For example, in Fig. 4b, the detected rotating axis in the northwest orientation triggers more salient Doppler shifts when we measure the dual-point noncoaxial RDSs at P1 and P4 residing on the positive x-axis and negative y-axis (i.e., these two shifts in the northwest orientation (or quadrant II) are larger than the frequency threshold fth simultaneously). The same principle is validated in Fig. 4c, d. These experimental results are consistent with the theoretical analyses. In practice, this remarkable phenomenon can be further implemented for highly sensitive and accurate detection of the rotating axis after the rotating axis orientation is estimated (through the cherry-picked dual points possessing frequency shifts greater than the frequency threshold simultaneously). This is because larger shifts can move away from the low-frequency noise domain, thereby leading to a significantly higher salient signal-to-noise ratio. Hence, the rotating axis in quadrants I, II, III, and IV could be accurately measured using four pairs of adjacent dual points: P3 and P4, P1 and P4, P1 and P2, and P2 and P3, respectively.
Fig. 4 Detection of the rotating axis orientation via other dual-point noncoaxial RDSs. Measured dual-point noncoaxial RDSs at points a P1 and P3; b P1 and P4; c P2 and P3; as well as d P3 and P4. The asterisks denote the measured values, whereas the solid lines indicate the theoretical predictions. The frequency threshold fth = 763.9 Hz (circular green-dotted line).
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As stated above, with an increase in the linearly coherent superposed light fields (i.e., N > 2 the Doppler peaks in the measured Doppler spectra become more complicated. Doppler peaks are induced by self- and cross-interference between different modal components of the OAM light. At this point, it becomes difficult to distinguish which Doppler peak corresponds to the prescribed OAM components, leading to an unclear discrimination of the rotating axis orientations. To address this issue, we propose the use of modal filters to sort specific modal components within the scattered light, allowing the detection of only a single Doppler signal peak. Consequently, by comparing the dual-point non-coaxial RDSs with the prescribed frequency threshold, the rotating axis can be unambiguously determined for arbitrarily synthesised OAM light fields.
Fig. 5a illustrates an experimental configuration of this general strategy to discriminate rotating axis orientations. The core elements in the proposed detection setup include a pair of optical modal filters, comprising two spatial light modulators (SLM1 and SLM2), two lenses (L5 and L6) as well as two avalanche photodetectors (PD1 and PD2). In practice, the lens can also be replaced by a single-mode optical fiber. The work principle of the optical modal filters is to measure the inner product (sometimes also called the projection measurement) between an incident light field and a loaded basis vector with orthogonality and completeness23-25. We respectively guide two arbitrary scattered hotspots that are modulated by a noncoaxially rotating surface with velocity Ω into the optical modal filters, and fiter out specific OAM modal components that arise from synthetic OAM light field EN. Last, we acquire the specific Doppler signals that possess time-varying phase shifts of lnΩt towards each of OAM eigenmodes by using the photodetectors. The detailed theoretical analyses are given in the Methods section. Here, we only filter out E0,±ln components and detect solely their Doppler signals, making the Doppler signal peak much simple and more recognizable. After obtaining two noncoaxial RDSs, we can further compare them with a prescribed frequency threshold related to ln, and thus the rotating axis orientations can be clearly discriminated.
Fig. 5 a Experimental arrangement of a general strategy for detecting rotating axis orientations via arbitrary emitted synthetic OAM light fields EN. Here, an arbitrarily synthetic OAM light field EN is launched noncoaxially to the rotating surface. Subsequently, two scattered Gaussian light spots are blocked with a triangular baffle (TB) before two additional Gaussian light spots are reflected by BS2 into a pair of modal filters. Because the two passed light spots are close, we here use a D-mirror to separate these spots into two paths. Subsequently, each path passes through a modal filter (SLM1 and SLM2 as well as L5 and L6) and the filtered signals are detected with an avalanche photodetector (PD), respectively. Finally, the detected analog signals are digitalized by an OSC and displayed on it. b–e Measured Doppler power spectra filtered from modal filters at dual points P1 (bluish solid lines) and P2 (reddish solid lines) by emitting a synthetic OAM light field $ {E}_{4}^{gs} $ with OAM indices of the geometric sequence ln = 2n+1. Where the rotating axis is preset within b quadrant I; c quadrant II; d quadrant III; and e quadrant. IV The frequency threshold fth =1528 Hz (green dotted lines) corresponding to ±16th-order OAM components.
As an example, we here select $ {E}_{4}^{gs} $ as the emitted light field (Fig. S1(g)) and $ {\mathrm{\Phi }}_{i}\left(r,\phi \right)={E}_{0,\pm 16} $ as basis vectors to synchronously acquire dual-point noncoaxial RDSs for the effective discrimination of rotating axis orientations. We maintain the axis distance and preset rotating speed constant, and alter the preset axis orientations from quadrants I to IV. Subsequently, we measured the Doppler signal spectra at two points of P1 and P2, respectively, as plotted in Fig. 5b–d. The Doppler signal peaks become single and much easier to be recognized. Therefore, we can discriminate the rotating axis orientations by comparing the corresponding dual-points RDS magnitudes and a frequency threshold. Note that the frequency threshold fth relates to the filtered OAM orders, which here is fth =1528 Hz corresponding to ±16th-order OAM components.
Similarly, the rotating axis orientations can also be discriminated by acquiring the noncoaxial RDSs at the other dual points. The simulated and measured results are shown in Fig. 6a–d, respectively. We can see that arbitrarily selected dual points can be used to detect the rotating axis orientations. The measured results are in good agreement with the theoretical simulations. Additionally, it is worth noting that as the filtered OAM orders increase, the matched dual-point noncoaxial RDSs also increase. Such an enlarged frequency shift by increasing N values of the emitted synthetic OAM light fields or the filtered OAM index in Eq. 6, can also be used for accurate discrimination of the rotating axis information. Additionally, the oppositely oriented rotating axes can also be sensitively and accurately discriminated by four pairs of adjacent dual points because of the further enlarged frequency shifts, leading to a salient signal-to-noise ratio, which is consistent with Fig. 4. Based on the discrimination approach proposed above, we accurately measured the rotating axis within full orientation. The meteorological results are shown in Fig. 6e. Each data point was measured 20 times, and the statistical values were used in the final result. We observed that the measured values were in perfect agreement with the prior-settled axis orientations. The maximum absolute measurement errors of the rotating axis orientations, which are principally derived from the limited frequency resolution, were extremely small at approximately 2.23°. This could be further reduced by increasing the sampling time. Overall, we proposed and demonstrated a more general strategy for rapidly and efficiently discriminating rotating-axis orientations.
Fig. 6 Noncoaxial RDSs for arbitrary dual points when rotating axis resides in full quadrants. a–d Emitting $ {E}_{4}^{gs} $ field and uploading ±16th-order OAM components onto two modal filters, and then measuring Doppler shifts at dual points a P1 and P2; b P1 and P4; c P2 and P3; d P3 and P4. The asterisks denote the measured values whereas the solid lines indicate the theoretical predications. e Accurate detection of full orientations of the rotating axis via particularly selected four pairs of adjacent dual-points when the rotating axis is prior-settled in distinct orientations. The frequency threshold fth = 1528 Hz (circular green dotted lines) corresponding to ±16th-order OAM components.
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In our case, two scattered Gaussian light spots were fed into optical modal filters. A Gaussian light spot $E\left( {r,\varphi } \right)$ can be represented by a set of orthogonal basis vectors ${\Phi _i}\left( {r,\varphi } \right)$:
$$ E\left( {r,\varphi } \right)\; = \sum\limits_i {{C_i}} {\Phi _i}\left( {r,\varphi } \right) $$ (4) After passing through optical modal filters, the on-axis intensity was calculated using the inner product of Eq. 4, and its square modulus was determined as follows:
$$ {\left| {{C_i}} \right|^2} = {\left| {\langle \Phi _i^*|E\rangle } \right|^2} = {\left| {\iint {\Phi _i^*}\left( {r,\varphi } \right)E\left( {r,\varphi } \right)rdrd\varphi } \right|^2} $$ (5) where the asterisk denotes the complex conjugate operation. In addition, the orthogonal basis vector ${\Phi _i}\left( {r,\varphi } \right)$ can be represented by multiple cases, such as OAM states, LG modes, or phase-conjugated superposition states. In our experiment, we preloaded the conjugate of the phase-conjugated superposition states onto the SLMs. This basis vector can be characterised as follows:
$$ {\Phi _i}\left( {r,\varphi } \right)\; = \;{E_{p, \pm {l_n}}} = \;{E_{p,{l_n}}} + {E_{p, - {l_n}}} $$ (6) with $p\; = \;0$. The projected light field intensity can then be measured using photodetectors, which characterise specific Doppler signals. It is worth noting that the Gaussian light spots arise from the customised light field EN, which is modulated by a non-coaxially rotating object with velocity $\Omega $, thus leading to a time-varying phase shift of lnΩt towards each of the OAM eigenmodes. Here, we only filter out the E0,±ln components and detect their Doppler signals, making the Doppler signal peak much simpler and more recognisable. After obtaining two non-coaxial RDSs, we can further compare them with a prescribed frequency threshold related to ln, thus, the rotating axis orientations can be clearly discriminated.
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To validate the effectiveness of the DNRDE scheme in determining rotating axis orientations in real time with high energy efficiency and high accuracy, a proof-of-principle experiment was conceived and conducted, as illustrated in Fig. S3. A single longitudinal-mode laser emitting a continuous-wave beam at 532 nm was coupled with a microobjective (MO) into a single-mode fibre (SMF) to generate a perfect Gaussian mode. The optical polarisation direction of the Gaussian mode was modulated horizontally using a linear polariser (LP), and a half-wave plate (HWP) is employed to control the output laser energy. The Gaussian mode is then reflected from a mirror (M) and passed through a phase-only spatial light modulator (SLM) loaded with a computer-generated hologram in advance, reshaping the mode into synthetic OAM light modes (Fig. S4(f) in the SI). Using a 4f system composed of two confocal lenses (L1 and L2) and an iris, first-order diffractive light with a high-quality synthetic OAM mode can be well filtered. This well-established mode is then split into two paths using a beam splitter (BS1). One path was utilised to register the generated light field distributions dynamically by exploiting a CCD combined with a focused lens (L3). The other was directed towards a noncoaxially rotating object surface (rotor) with a rotating velocity of Ω. Subsequently, the backscattered light from the object is reflected by another beam splitter (BS2) and focused selectively onto two single-mode optical fibres combined with the corresponding single-point avalanche photodetectors (APD1 and APD2) to gather dual-point echo light signals32. In this experiment, the analogue signals were converted into discrete digital counterparts using an oscilloscope (OSC) linked to the photodetectors via cables. The detected echo signals were displayed in real time on a personal computer (PC) connected to the OSC and used to implement the associated digital signal post-processing. It is worth mentioning that signal processing consisted of two key steps: performing the discrete Fourier transform (DFT) for the time sequences and denoising together with smoothing by combining the spectral subtraction method and a digitally encoded Wiener filter. Details of the postprocessing are provided in Supplementary Note 5 of the SI. Eventually, the dual-point noncoaxial RDSs acquired by post-processing can be employed to accurately ascertain the rotating axis orientations.
Dual-point noncoaxial rotational Doppler effect towards synthetic OAM light fields for real-time rotating axis detection
- Light: Advanced Manufacturing 4, Article number: (2023)
- Received: 29 May 2023
- Revised: 08 August 2023
- Accepted: 10 August 2023 Published online: 26 September 2023
doi: https://doi.org/10.37188/lam.2023.027
Abstract: Probing the axis of a rotator is important in astrophysics, aerospace, manufacturing, machinery, automation, and virtual reality, etc. Existing optical solutions commonly require multiple sequential measurements via symmetry-broken light fields, which make them time-consuming, inefficient, and prone to accumulated errors. Herein, we propose the concept of a dual-point noncoaxial rotational Doppler effect (DNRDE) and demonstrate a one-shot detection technique to solve this problem. An on-demand synthetic orbital angular momentum (OAM) light beam impinges on a rotating scatterer surface, supporting dual-point rotational Doppler shifts, in which the information of the rotating axis is acquired by comparing these two frequency shifts with a prescribed threshold. The existence of arbitrary dual-point Doppler shifts enables the one-time direct identification of rotating axis orientations, which is fundamentally inaccessible in single-point detection. This robust detection technique is compatible with generalised synthetic OAM light fields by utilising optical modal filters. Compared with traditional approaches, our DNRDE-driven detection approach exhibits a four-fold enhancement in measurement speed, higher energy efficiency, and superior accuracy with a maximal absolute measurement error of 2.23°. The proposed dual-point detection method holds great promise for detecting rotating bodies in various applications, such as astronomical surveys and industrial manufacturing.
Research Summary
Laser Doppler effect: dual-point detection enables real-time rotating axis recognition
Probing rotating axis holds a huge promise for industrial manufacturing, vehicle detection, and recognition of a rotary body. However, the existing optical approaches that require multiple measurements typically are time-consuming, inefficient and inevitably undergo salient measurement error. To overcome these issues, a dual-point noncoaxial rotational Doppler effect and a versatile discrimination technique for real-time rotating-axis recognition are developed and demonstrated. This scheme combines the advantages of the coherent superposition strategy along with optical modal filters and the dual-point Doppler metrology, enabling real-time, efficient, and high-accuracy detections of the information of full rotating-axis orientations. The prototype optical system demonstrated in this paper can be further applied in rotational Doppler LiDAR.
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