基于可观测性分析的单测角相对导航与闭环制导技术

doi:10.7527/S1000-6893.2014.0301

Abstract

Abstract:

Aimed at the problem of space rendezvous using angles-only measurements, relative navigation integrated with closed-loop guidance is developed based on observability analysis. Firstly, the systemic filtering model is established, based on which the observability is investigated from a novel prospect and the observable condition is obtained. Then, integrated with multi-pulse sliding safe guidance strategy, the coupling relationship between angles-only relative navigation and guidance is analyzed and the mathematical expressions are obtained. After that, the integrated scheme of relative navigation and closed-loop guidance is designed by using the coupling expresses. Finally, Monte Carlo simulations are conducted to validate the approach and the performance of navigation and guidance with different accuracies of sensor and initial relative states is analyzed.

Key words: observability analysis, Monte Carlo method, angles-only, navigation, guidance, autonomous rendezvous

CLC Number:

V448

GONG Baichun, LUO Jianjun, YUAN Jianping, MA Weihua. Angles-only relative navigation integrated with closed-loop guidance technology based on observability analysis[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2015, 36(7): 2411-2419.

References

[1] Liang B, Du X D, Li C, et al. Advances in space robot on-orbit servicing for non-cooperative spacecraft[J]. Robot, 2012, 34(2): 242-256(in Chinese). 梁斌, 杜晓东, 李成, 等. 空间机器人非合作航天器在轨服务进展研究[J]. 机器人,2012, 34(2): 242-256.
[2] Tatsch A, Fitz-Coy N, Gladun S. On-orbit servicing: a brief survey[C]//Performance Metrics for Intelligent Systems Conference, 2006.
[3] Charles F L. On-orbit servicing for future space observatories, AIAA-2005-6609[R]. Reston: AIAA, 2005.
[4] Fehse W. Automated rendezvous and docking of spacecraft[M]. Cambridge: Cambridge University Press, 2003: 243-282.
[5] Chari R J. Autonomous orbital rendezvous using angles-only navigation[D]. Boston: Massachusetts Institute of Technology, 2001.
[6] Woffinden D C. Angles-only navigation for autonomous orbital rendezvous[D]. Logan: Utah State University, 2008.
[7] Woffinden D C, Geller D K. Relative angles-only navigation and pose estimation for autonomous orbital rendezvous[J]. Journal of Guidance, Control, and Dynamics, 2007, 30(5): 1455-1469.
[8] Woffinden D C, Geller D K. Optimal orbital rendezvous maneuvering for angles-only navigation[J]. Journal of Guidance, Control, and Dynamics, 2009, 32(4): 1382-1387.
[9] Li J R, Li H Y, Tang G J. Research on the strategy of angles-only relative navigation for autonomous rendezvous[J]. SCIENCE CHINA Technological Sciences, 2011, 54(7): 1865-1872.
[10] Grzymisch J, Ficher W. Observability criteria and unobservable maneuvers for in-orbit bearings-only navigation[J]. Journal of Guidance, Control, and Dynamics, 2014, 37(4): 1250-1259.
[11] Grzymisch J, Fehse W, Ficher W, et al. On the issues and requirements of bearing-only of guidance and navigation[C]//Proceedings of 64th IAC, 2013.
[12] Gaias G, D'Amico S, Ardaens J S. Angles-only navigation to a noncooperative satellite using relative orbital elements[J]. Journal of Guidance, Control, and Dynamics, 2014, 37(2): 439-451.
[13] Clohessy W H, Wiltshire R S. Terminal guidance system for satellite rendezvous[J]. Journal of Astronautical Sciences, 1960, 27(9): 653-678.
[14] Okasha M, Newman B. Guidance, navigation and control for satellite proximity operations using Tschauner-Hempel equations[J]. Journal of Astronautical Sciences, 2013, 60(1): 109-136.
[15] Qin Y Y, Zhang H Y, Wang S H. Kalman filter and integrated navigation theory[M]. Xi'an: Northwestern Polytechnical University Press, 1998: 34-35 (in Chinese). 秦永元, 张洪钺, 汪叔华. 卡尔曼滤波与组合导航原理[M]. 西安: 西北工业大学出版社, 1998: 34-35.

Angles-only relative navigation integrated with closed-loop guidance technology based on observability analysis

PDF (PC)

Knowledge

Abstract

Cite this article

share this article

References

Related Articles 15

Recommended Articles

Metrics

Comments

[1]	Jiaxiang LI, Jianhua CHENG, Liang LI, Zhibo NA, Chun JIA. Troposphere anomaly integrity monitoring parameters for GBAS [J]. Acta Aeronautica et Astronautica Sinica, 2024, 45(7): 328817-328817.
[2]	Jing ZHAO, Dan SONG. Integrity monitoring method for GNSS/IMU integrated navigation system of UAV [J]. Acta Aeronautica et Astronautica Sinica, 2024, 45(7): 328943-328943.
[3]	Wei ZHENG, Yusong WANG, Kun JIANG, Yidi WANG. Space experiments on X-ray pulsar navigation: Progress and prospects [J]. Acta Aeronautica et Astronautica Sinica, 2024, 45(6): 28843-028843.
[4]	Weiping YANG. Development trend of navigation guidance and control technology for new generation aircraft [J]. Acta Aeronautica et Astronautica Sinica, 2024, 45(5): 529720-529720.
[5]	Weiqing LAI, Jiuqing WAN. Distributed relative positioning of aircraft group based on path⁃sum algorithm [J]. Acta Aeronautica et Astronautica Sinica, 2024, 45(4): 328735-328735.
[6]	Haiqiao LIU, Meng LIU, Zichao GONG, Jing DONG. A review of image matching methods based on deep learning [J]. Acta Aeronautica et Astronautica Sinica, 2024, 45(3): 28796-028796.
[7]	Zhichuan HE, Jiang WANG, Shipeng FAN, Peng WANG, Miao HOU. Three-dimensional cooperative guidance with field-of-view constraints based on event-triggered mechanism [J]. Acta Aeronautica et Astronautica Sinica, 2024, 45(3): 328687-328687.
[8]	Ruijie LI, Liang LI, Jiachang JIANG, Li CHENG, Liuqi WANG. RAIM integrity risk estimation method based on worst multi⁃satellite faults searching [J]. Acta Aeronautica et Astronautica Sinica, 2024, 45(2): 328684-328684.
[9]	Yanbo ZHU, Zhipeng WANG, Kai GUO, Zhiqiang DAN. L-band digital aeronautical communications system development status and challenges [J]. Acta Aeronautica et Astronautica Sinica, 2024, 45(10): 29161-029161.
[10]	Hongyan ZHANG, Wei WANG, Shiwei CHEN, Yi JI, Jiaqi LIU. Integrated guidance and control design based on fully actuated system method [J]. Acta Aeronautica et Astronautica Sinica, 2024, 45(1): 628891-628891.
[11]	Ziyi WU, Shaoming HE, Yadong WANG, Hongyan LI. Nonlinear observability-enhancement optimal guidance law for moving targets [J]. Acta Aeronautica et Astronautica Sinica, 2023, 44(S2): 729750-729750.
[12]	Zhefeng YU, Shichang LIANG, Weibo SHI, Deyang TIAN, Anhua SHI, Dongjun LIAO, Ying YANG. Analysis and evaluation technology for optical radiation and radar scattering characteristics of HTV⁃2⁃like vehicle [J]. Acta Aeronautica et Astronautica Sinica, 2023, 44(S2): 729465-729465.
[13]	Jing NI, Bo MA, Zhaoxu YANG, Chenggang TAO, Yan ZHOU, Yiwen HU. Design and test of visual-inertial integrated method for landing guidance [J]. Acta Aeronautica et Astronautica Sinica, 2023, 44(S1): 727636-727636.
[14]	Yusong WANG, Yidi WANG, Wei ZHENG. Solar information assisted pulse phase estimation method and navigation application [J]. Acta Aeronautica et Astronautica Sinica, 2023, 44(S1): 727651-727651.
[15]	Fengzhu CHE, Changwei MI, Haoping ZHANG, Xin ZHANG. High precision navigation system of cooperative aerial bomb based on scalar processing [J]. Acta Aeronautica et Astronautica Sinica, 2023, 44(S1): 727632-727632.