Time-varying modal parameters identification of large flexible spacecraft using a recursive algorithm
文献类型:期刊论文
作者 | Ni ZY(倪智宇); Wu ZG(吴志刚); Wu SN(邬树楠) |
刊名 | International Journal of Aeronautical and Space Sciences
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出版日期 | 2016 |
卷号 | 17期号:2页码:184-194 |
关键词 | modal parameter identification large flexible spacecraft linear time-varying system recursive subspace algorithm |
ISSN号 | 2093-274X |
产权排序 | 1 |
通讯作者 | 吴志刚 |
中文摘要 | In existing identification methods for on-orbit spacecraft, such as eigensystem realization algorithm (ERA) and subspace method identification (SMI), singular value decomposition (SVD) is used frequently to estimate the modal parameters. However, these identification methods are often used to process the linear time-invariant system, and there is a lower computation efficiency using the SVD when the system order of spacecraft is high. In this study, to improve the computational efficiency in identifying time-varying modal parameters of large spacecraft, a faster recursive algorithm called fast approximated power iteration (FAPI) is employed. This approach avoids the SVD and can be provided as an alternative spacecraft identification method, and the latest modal parameters obtained can be applied for updating the controller parameters timely (e.g. the self-adaptive control problem). In numerical simulations, two large flexible spacecraft models, the Engineering Test Satellite-VIII (ETS-VIII) and Soil Moisture Active/Passive (SMAP) satellite, are established. The identification results show that this recursive algorithm can obtain the time-varying modal parameters, and the computation time is reduced significantly. |
WOS标题词 | Science & Technology ; Technology |
类目[WOS] | Engineering, Aerospace |
研究领域[WOS] | Engineering |
关键词[WOS] | ETS-VIII ; SYSTEM ; CONTROLLER |
收录类别 | SCI ; EI |
语种 | 英语 |
WOS记录号 | WOS:000379716000006 |
源URL | [http://ir.sia.cn/handle/173321/18730] ![]() |
专题 | 沈阳自动化研究所_空间自动化技术研究室 |
推荐引用方式 GB/T 7714 | Ni ZY,Wu ZG,Wu SN. Time-varying modal parameters identification of large flexible spacecraft using a recursive algorithm[J]. International Journal of Aeronautical and Space Sciences,2016,17(2):184-194. |
APA | Ni ZY,Wu ZG,&Wu SN.(2016).Time-varying modal parameters identification of large flexible spacecraft using a recursive algorithm.International Journal of Aeronautical and Space Sciences,17(2),184-194. |
MLA | Ni ZY,et al."Time-varying modal parameters identification of large flexible spacecraft using a recursive algorithm".International Journal of Aeronautical and Space Sciences 17.2(2016):184-194. |
入库方式: OAI收割
来源:沈阳自动化研究所
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