多刚体卫星转动惯量在轨辨识

doi:10.3969/j.issn.1674-1579.2015.06.007

Abstract

Abstract: Accurate dynamics characteristics are important for rotary inertia identification. Considering the effect of solar cell array rotation in dynamics, a method of inertia identification is proposed, which is applied to identify the body inertia and solar cell array inertia simultaneously. Thinking of the coupling between the variables, the optimized identification model with constraint is deduced based on the modeled multibody attitude dynamics. The precise solution is achieved via the algorithm of constraint least squares. Finally, the feasibility of the identification method is verified by simulation and calculation.

Key words: multibody attitude dynamics, rotary inertia identification, constraint least squares

CLC Number:

XU Ying, 吕Wang , LI Yun-Duan, ZHANG Da-Wei. Identification of Rotary Inertia for MultiBody Satellite[J]., 2015, 41(6): 31-.

0
/ / Recommend

Add to citation manager EndNote|Reference Manager|ProCite|BibTeX|RefWorks

URL: http://journal01.magtech.org.cn/Jwk3_kjkzjs/EN/10.3969/j.issn.1674-1579.2015.06.007

http://journal01.magtech.org.cn/Jwk3_kjkzjs/EN/Y2015/V41/I6/31

References

［1］BERGMANN E V, WALKER B K, LEVY D R. Mass property estimation for control asymmetrical satellite［J］. Journal of Guidance, Control and Dynamics, 1987, 10(2): 483492. ［2］EDWARD W, CHRIS L, ROBERT W M. Online gyrobased mass property identification for thruster controlled spacecraft using recursive least squares［C］//Proceedings of the 45th IEEE International Midwest Symposium on Circuits and systems. New York:IEEE, 2002: 14. ［3］EDWARD W, SUTTER D W, MAH R W. Motion based on mass and thruster property identification for thruster controlled spacecraft［C］//Proceedings of the AIAA Infotech@Aerospace Conference. Washington D.C.: AIAA, 2005: 140.［4］TANYGIN S, WILLIAMS T. Mass property estimation using coasting maneuvers［J］. Journal of Guidance, Control and Dynamics. 1997, 20(4): 625632. ［5］WILSON E. Multiple concurrent recursive least squares identification with application to online spacecraft massproperty identification［P］. Redwood City, US 7110915B2. 2006. ［6］王书廷,曹喜滨.卫星质量特性的在线辨识算法研究［C］//第25届中国控制会议论文集.北京：中国自动化学会,2006: 519524. WANG S T, CAO X B. Online massproperty identification algorithm research for satellite［C］//Proceedings of the 25th Chinese Control Conference. Beijing: CAA, 2006: 519524. ［7］黄河, 周军, 刘莹莹. 航天器转动惯量在线辨识［J］. 系统仿真学报, 2010, 22(5): 11171120. HUANG H, ZHOU J, LIU Y Y. Online Identification of Spacecraft Moment of Inertia［J］. Journal of System Simulation, 2010, 22(5): 11171120. ［8］荆武兴，韦文书，高长胜.基于陀螺测量信息的航天器突变参数识别方法［J］.系统工程与电子技术，2013,35(9):19281932. XING W X, WEI W S, GAO CS. Identification of the mutation parameters for the spacecraft based on gyros［J］. Systems Engineering and Electronics 2013, 35(9): 19281932. ［9］徐文福,何勇,王学谦等. 航天器质量特性参数的在轨辨识方法［J］.宇航学报,2010,31(8):19071914. XU W F, HE Y, WANG X Q, et al. On Orbit identification of mass characteristic parameters for spacecraft［J］. Journal of Astronautics, 2010, 31(8): 19071914. ［10］章仁为.卫星轨道姿态动力学与控制［M］. 北京航空航天大学出版社. 1998 ［11］GILL P E, MURRAY W, WRIGHT M H. Practical optimization［M］. London: Academic Press, 1981.

[1]	HUANG Jian-Bin, HUANG Long-Fei, HAN Xu, MENG Bo, LI Zhi, WANG Wen-Long, LI Wen. [J]. , 2018, 44(5): 30-37.
[2]	HAN Dong, HUANG Pan-Feng, LIU Xi-Yao. [J]. , 2018, 44(5): 38-46.
[3]	LIU Miao, LI Zhong-Kui. [J]. , 2018, 44(5): 47-54.
[4]	SUN Yun-Long, YUAN Chang-Qing, LI Zheng-Guang. [J]. , 2018, 44(4): 16-25.
[5]	HU Jin-Chang, ZHANG Hong-Hua, WANG Ze-Guo, CHEN Shang-Shang. [J]. , 2018, 44(4): 56-60.
[6]	SU Shao-Kan, PENG Bo, WANG Li-Wei, ZHENG Wei, CHANG Tao, CHEN Ming-Yang. [J]. , 2018, 44(4): 72-78.
[7]	ZHAO Shuang, ZHANG Ya-Sheng, DAI Hua-Yu, QI Yue- . Failure Performance and Reconstruction Method of Satellite Navigation System [J]. , 2018, 44(2): 49-55.
[8]	SUN Xiu-Qing, ZHANG Du-Zhou, WANG Li, WU Fen-Zhi. An Improved Method of Projector Calibration [J]. , 2018, 44(2): 62-66.
[9]	WANG Tong-Lei, CHEN Chao-Hui- . A Method of Analyzing and Localizing Software Vulnerability Automatically [J]. , 2018, 44(2): 73-78.
[10]	SUI Jie, CHENG Hui-Yan, YU Cheng-Wu, WU Yan-Peng, WANG Xiao-Yan, ZHENG Ran. A Thermal Stability Analysis and Simulation Method for Boresight Axis of Star Sensor [J]. , 2017, 43(4): 37-41.
[11]	LI Tao, WU Yun. Measurement Technology Based on Stereo Vision for NonCooperative Targets [J]. , 2017, 43(4): 52-56.
[12]	WU Fen-Zhi, GUO Shao-Gang, ZHU Fei-Hu, WANG Li, WU Yun, LIU Da. TwoStep Calibration Method of Lidar Sensor Based on Calibration Field [J]. , 2017, 43(4): 57-62.
[13]	CHEN Jian-Feng, YU Cheng-Wu, CHENG Hui-Yan, SUI Jie, WU Yan-Peng. An Optimal Design of Star Tracker Baffle Based on Bipod Structure [J]. , 2017, 43(4): 68-72.
[14]	CHENG Hui-Yan, ZHONG Hong-Jun, WANG Long, YANG Jun, ZHENG Ran. A Fast Algorithm of AllSky Star Map Automated Identification [J]. , 2017, 43(4): 73-78.
[15]	WANG Fei, YUAN Jian-Ping, YUAN Jing. Formation Keeping and Reconfiguration for Solar Sail Spacecraft [J]. , 2017, 43(3): 7-14.

Identification of Rotary Inertia for MultiBody Satellite

PDF (PC)

Like

Knowledge

Abstract

Cite this article

share this article

References

Related Articles 15

Metrics

Comments

Recommended 0