Dual-spacecraft formation flying in deep space: Optimal collision-free reconfigurations

被引：28

作者：

Kim, YS

Mesbahi, M

Hadaegh, FY

机构：

[1] Univ Washington, Dept Aeronaut & Astronaut, Seattle, WA 98195 USA

[2] CALTECH, Jet Prop Lab, Auton & Control Sect, Pasadena, CA 91109 USA

来源：

JOURNAL OF GUIDANCE CONTROL AND DYNAMICS | 2003年 / 26卷 / 02期

关键词：

D O I：

10.2514/2.5059

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

The optimal collision-free reconfiguration for a dual-spacecraft system as a state constrained optimal control problem is considered. It is often the case that such a problem formulation and the ensuing necessary optimality conditions do not lead to efficiently computable optimal control forces. As such, a solution to the dual-spacecraft optimal collision-free reconfiguration by relying on this approach is provided.

引用

页码：375 / 379

页数：5

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