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作 者:Hao Liu Deyuan Liu Ming Cheng
机构地区:[1]Institute of Articial Intelligence,Beihang University,Beijing 100191,P.R.China [2]School of Astronautics,Beihang University,Beijing 100191,P.R.China [3]School of Automation Science and Electrical Engineering,Beihang University,Beijing 100191,P.R.China
出 处:《Guidance, Navigation and Control》2021年第4期26-47,共22页制导、导航与控制(英文)
基 金:supported by the National Natural Science Foundation of China under Grant 61873012.
摘 要:In this paper,the fault-tolesant attitude aynchronisation aontrol problem for a team of bet-soganua man leatellita in addrsed,subject to multaple actuator faulta and uneertainties in the satellite dynamles.A fully distributed adapSe fault-tokerant controlker,completely inde pendently of the knowledge of the gobal infarmation,is propoaed to achieve the desired attstude aynchranlatin.The attitade tracking aror of the glohal clased-loop eantrol aystem is paoven to onverge into a givan naighborbood of the origin ultimately.Simmlation rasults are givan to validate the afectivenas and advantaga of the propased adaptive controller dor the belerogenaou satellite formation flying team,against the infuenoe of actuator faults and umeertaintin.
关 键 词:Cooperative control adaptive control uncertain system nonlinear system heterogenous minisatellites
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