Modeling and analysis of pointing error for non-landing vehicle-mounted photoelectric theodolite

Qingjia Gao , Chong Wang , Yanjun Liu , Xiaoming Wang , Tongbang Wu , Haoyuan Zhang

Optoelectronics Letters ›› 2024, Vol. 20 ›› Issue (5) : 294 -298.

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Optoelectronics Letters ›› 2024, Vol. 20 ›› Issue (5) : 294 -298. DOI: 10.1007/s11801-024-3159-5
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Modeling and analysis of pointing error for non-landing vehicle-mounted photoelectric theodolite

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Abstract

In order to achieve high accuracy measurement for non-landing vehicle-mounted photoelectric theodolite (NVPT) with continuous zoom optical system, a theoretical model of pointing error is presented. Starting with the working mode, the error source of the whole closed loop which affects the pointing error is analyzed. The measurement equation is derived using a coordinate transformation. The pointing error model is then obtained with the help of Monte Carlo method. The error of an NVPT prototype is measured, showing that the pointing error can be predicted accurately. A high precision NVPT with continuous zoom optical system is successfully designed and analyzed, with an accuracy of 11.9″ at azimuth and 10.9″ at elevation, when the optical focal length is set between 1 000 mm and 4 000 mm.

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Qingjia Gao, Chong Wang, Yanjun Liu, Xiaoming Wang, Tongbang Wu, Haoyuan Zhang. Modeling and analysis of pointing error for non-landing vehicle-mounted photoelectric theodolite. Optoelectronics Letters, 2024, 20(5): 294-298 DOI:10.1007/s11801-024-3159-5

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References

[1]

YuY, LiuZ Y, SunZ Y, et al.. Development status and prospect of photoelectric measurement equipment in test range. Acta optica sinica, 2023, 43(6):0600002[J]

[2]

ZhangS J, GaoY G, XueX Y, et al.. Design and functional test of a novel optical testing. Optoelectronics letters, 2018, 14(6): 461-464 J]

[3]

LuoJ, XuP, PanN, et al.. Non-landing vehicle-mounted electro-optical theodolite deformation measurement method using inertial sensors. Measurement science and technology, 2019, 30: 055103 J]

[4]

XieM L, MaC W, LiuK, et al.. The application of active polarization imaging technology of the vehicle theodolite. Optics communications, 2019, 433: 74-80 J]

[5]

LuoJ, FanY K, JiangP, et al.. Vehicle platform attitude estimation method based on adaptive Kalman filter and sliding window least squares. Measurement science and technology, 2021, 32: 035007 J]

[6]

HeY, ZhangY H, FengX H, et al.. Pointing error correction for a moving-platform electro-optical telescope using an optimized parameter model. Sensors, 2023, 23: 4121 J]

[7]

GaoQ J, WangC, WangQ L, et al.. Stability research of supporting platform used for vehicle-mounted optoelectronic theodolite. Acta optica sinica, 2023, 43(21):2112004[J]

[8]

LiuJ P, ZhangX H, LiuH B, et al.. Correction method for non-landing measuring of vehicle-mounted theodolite based on static datum conversion. Science China technological sciences, 2013, 56(9): 2268-2277 J]

[9]

ZhengX H, WeiZ Z, ZhangG J. Global calibration of unleveled theodolite using angular distance constraints. Applied optics, 2016, 55(33):9495-9503 J]

[10]

LouY M, HuJ M. Coordinate transformation of three-dimensional image in integral imaging system illuminated by a point light source. Optik, 2021, 226: 165885 J]

[11]

ZhangH W, LiP F. Measurement-driven Gauss-Hermite particle filter with soft spatiotemporal constraints for multi-optical theodolites target track-ing. Chinese journal of aeronautics, 2023, 36(8):313-330 J]

[12]

GaoQ J, SunQ, QuF, et al.. Line-of-sight rate modeling and error analysis of inertial stabilized platforms by coordinate transformation. Journal of engineering manufacture, 2019, 233(4):1317-1332 J]

[13]

HuangB, LiZ H, TianX Z, et al.. Modeling and correction of pointing error of space-borne optical im-ager. Optik, 2021, 247: 167998 J]

[14]

XiaoF Z, ChenL Q. Fully actuated systems in terms of quaternions for spacecraft attitude control. Acta astronautica, 2023, 209: 1-5 J]

[15]

HongH J, ZhangZ Y. Modeling and calibration of pointing errors using a semi-parametric regression method with applications in inertially stabilized platforms. Journal of engineering manufacture, 2013, 227(10):1492-1503 J]

[16]

ZhouX Y, MaD X, FanD P, et al.. Error analysis of mast mounted electro-optical stabilized platform based on multi-body kinematics theory. Proceedings of SPIE, 2011, 7544: 75446R J]

[17]

WangJ Q, JinG, YangX B. Optical instrument overall design, 2022, Beijing, National Defense Industry Press: 149-187[M]

[18]

YangT W, ZhangZ Z. Optical-electronic measurement theory and method in flight test, 2014, Beijing, National Defense Industry Press: 89-93[M]

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