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 |
DOI | 10.1117/12.2309650 |
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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文件名称/大小 | 文献类型 | 版本类型 | 开放类型 | 使用许可 | ||
Simulation Design of(509KB) | 会议论文 | 限制开放 | CC BY-NC-SA | 请求全文 |
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