中国科学院机构知识库网格
Chinese Academy of Sciences Institutional Repositories Grid
On-orbit identification of time-varying moment of inertia for spacecraft using an improved recursive subspace method

文献类型:会议论文

作者Ni ZY(倪智宇); Shen XH(沈昕慧); Liu JG(刘金国); Chang CG(畅晨光)
出版日期2017
会议名称2017 IEEE International Conference on Cybernetics and Intelligent Systems (CIS) and IEEE Conference on Robotics, Automation and Mechatronics (RAM)
会议日期November 19-21, 2017
会议地点Ningbo, China
关键词moment of inertia recursive subspace method time-varying system state-space model on-orbit identification
页码219-224
通讯作者Ni ZY(倪智宇)
中文摘要A large amount of data are required for the recursive predictor-based subspace identification (RPBSID) algorithm when system state vector is estimated. In this paper, an improved RPBSID method is presented and applied to identify the spacecraft time-varying moment of inertia parameters. Comparing with the original RPBSID algorithm, the improved method does not need to construct the corresponding Hankel matrix for each time instant when solving the state vector. The recursive least squares is used to implement the recursive estimation of the state vector, thereby reducing the computation cost of the identification process. Then, the moment of inertia matrix parameters can be determined recursively from the system state-space model by matrix transformation. In numerical simulations, for a spacecraft with flexible appendages, three cases that may cause the moments of inertia to change with time are investigated. The simulation results illustrate that the proposed recursive method can identify the time-varying moment of inertia parameters effectively and has higher computational efficiency than that of classical RPBSID algorithm.
收录类别EI ; CPCI(ISTP)
产权排序1
会议录2017 IEEE International Conference on Cybernetics and Intelligent Systems (CIS) and IEEE Conference on Robotics, Automation and Mechatronics (RAM)
会议录出版者IEEE
会议录出版地New York
语种英语
ISSN号2326-8239
ISBN号978-1-5386-3135-5
WOS记录号WOS:000425928100039
源URL[http://ir.sia.cn/handle/173321/21315]  
专题沈阳自动化研究所_空间自动化技术研究室
作者单位1.School of Mechanical Engineering and Automation, Northeastern University, Shenyang 110819, China
2.School of Mechanical Engineering and Automation, Northeastern University, Shenyang 110819, China
3.State Key Laboratory of Robotics, Shenyang Institute of Automation, Chinese Academy of Sciences, Shenyang 110016, China
4.State Key Laboratory of Robotics, Shenyang Institute of Automation, Chinese Academy of Sciences, Shenyang 110016, China
推荐引用方式
GB/T 7714
Ni ZY,Shen XH,Liu JG,et al. On-orbit identification of time-varying moment of inertia for spacecraft using an improved recursive subspace method[C]. 见:2017 IEEE International Conference on Cybernetics and Intelligent Systems (CIS) and IEEE Conference on Robotics, Automation and Mechatronics (RAM). Ningbo, China. November 19-21, 2017.

入库方式: OAI收割

来源:沈阳自动化研究所

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