Analysis of formation flying control of a pair of nanosatellites

被引：6
|
作者：
Veres, SM [1 ]
Gabriel, SB
Mayne, DQ
Rogers, E
机构：
[1] Univ Southampton, Sch Engn Sci, Astronaut Grp, Highfield SO17 1BJ, England
[2] Univ London Imperial Coll Sci Technol & Med, Dept Elect & Elect Engn, London SW7 2ZA, England
[3] Univ Southampton, Imperial Coll Sci & Technol, Dept Elect & Comp Sci, Highfield SO17 1BJ, England
来源：
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS | 2002年 / 25卷 / 05期
关键词：
D O I：
10.2514/2.4971
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
The generalized method for approximating complex polytopes in the state-space of satellite orbital dynamics is described. It is shown how this procedure may be used to compute approximate controllability sets and how these sets may, in turn, be used to obtain a nonlinear controller that robustly steers any initial state to a specified target set and thereafter maintains the state in the target set despite the disturbance.
引用
收藏
页码：971 / 974
页数：4
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