Spacecraft formation stabilization and fault tolerance: A state-varying switched system approach
نویسندگان
چکیده
The focus of this paper is the spacecraft formation flying problem where the formation switches successively among multiple shapes, the number and the composition of spacecraft in the group may change among these shapes, and some spacecraft may be faulty. The whole flying process is modeled as a state-varying switched system. The formation stability and fault tolerability are analyzed by using new results on state-varying switched systems.
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عنوان ژورنال:
- Systems & Control Letters
دوره 62 شماره
صفحات -
تاریخ انتشار 2013