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Simulation Design of Space Target Tracking System based on Radial Motion Principle
Yang, Yong-qing1; Liu, Peng1,2; Shen, Wen-ji1; Han, Jun-feng1; Liu, P (reprint author), Chinese Acad Sci, Xian Inst Opt & Precis Mech, Xian 710119, Shaanxi, Peoples R China.
2018
会议名称4th Seminar on Novel Optoelectronic Detection Technology and Application
会议录名称FOURTH SEMINAR ON NOVEL OPTOELECTRONIC DETECTION TECHNOLOGY AND APPLICATION
卷号10697
会议日期2017-10-24
会议地点Nanjing, PEOPLES R CHINA
出版地BELLINGHAM
出版者SPIE-INT SOC OPTICAL ENGINEERING
产权排序1
摘要

To support the planning of satellite orbit tracking and imaging experiment, and provide effective data for in-orbit test planning, the semi-physical simulation model of ground target tracking is established to simulate the target tracking process. First, this paper analyzes the typical work process of space target tracking system, established the spatial coordinates model of the space target LOS and satellite rendezvous process. Secondly, the mapping relationship between space target motion and tracking system is studied based on the principle of space radial motion principle. The semi-physical simulation's design principle and the system design scheme of space tracking are given by establishing the radial motion model of the target motion and tracking system. Finally, based on the analysis of the typical space target motion and the design of the semi physical simulation system, the simulation of the space target tracking process with the intersection distance of 60km and the moving speed of 4.2km/s is carried out. The simulation results show that This system can realize continuous tracking of space targets, when the system is stable, the miss distance is less than 0.5 pixels, Azimuth tracking velocity stability is 0.0174 degrees/s, the pitch tracking velocity stability is 0.0161 degrees/s. The test shows that the design principle of the simulation system is correct, and the closed-loop control process can be simulated effectively. This test can provide effective data supports for program analysis and control methods on orbit test, real-time monitoring, analysis and test of synchronous control countermeasures of fault verification.

关键词Radial Motion Principle Space Target Tracking In-orbit Test Semi-physical Simulation
学科领域Engineering, Electrical & Electronic
作者部门光电测量技术实验室
DOI10.1117/12.2309650
收录类别EI
ISBN号978-1-5106-1948-7
语种英语
ISSN号0277-786X
EI入藏号20182805539953
引用统计
文献类型会议论文
条目标识符http://ir.opt.ac.cn/handle/181661/30394
专题光电跟踪与测量技术研究室
通讯作者Liu, P (reprint author), Chinese Acad Sci, Xian Inst Opt & Precis Mech, Xian 710119, Shaanxi, Peoples R China.
作者单位1.Chinese Acad Sci, Xian Inst Opt & Precis Mech, Xian 710119, Shaanxi, Peoples R China.
2.Univ Chinese Acad Sci, Xian 710119, Shaanxi, Peoples R China
推荐引用方式
GB/T 7714
Yang, Yong-qing,Liu, Peng,Shen, Wen-ji,et al. Simulation Design of Space Target Tracking System based on Radial Motion Principle[C]. BELLINGHAM:SPIE-INT SOC OPTICAL ENGINEERING,2018.
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