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作者机构:Dalhousie Univ Halifax NS B3J 1Z1 Canada Univ Toronto Inst Aerosp Studies Toronto ON M3H 5T6 Canada
出 版 物:《JOURNAL OF GUIDANCE CONTROL AND DYNAMICS》 (J Guid Control Dyn)
年 卷 期:1999年第22卷第6期
页 面:908-909页
核心收录:
学科分类:12[管理学] 1201[管理学-管理科学与工程(可授管理学、工学学位)] 08[工学] 0804[工学-仪器科学与技术] 0825[工学-航空宇航科学与技术]
主 题:Flexible Structures Eigensystem Realization Algorithm Model Order Reduction Reaction Wheels Control System Design Space Structures Satellites Yaw
摘 要:Consideration is given to a novel approach to system identification that applies cubic smoothing splines to the system Markov parameters calculated by Observer Kalman Filter Identification. Applying this smoothing procedure early in the identification process allows models that are both low order and accurate to be directly identified. Experiments with Daisy, a flexible spacecraft emulator, demonstrate significant computational savings and numerical robustness by avoiding the model overspecification and reduction process. (AIAA)