State feedback H-infinity-suboptimal control of a rigid spacecraft

被引：56

作者：

Dalsmo, M ^{[1
]}

Egeland, O ^{[1
]}

机构：

[1] NORWEGIAN UNIV SCI & TECHNOL, DEPT ENGN CYBERNET, N-7034 TRONDHEIM, NORWAY

来源：

IEEE TRANSACTIONS ON AUTOMATIC CONTROL | 1997年 / 42卷 / 08期

关键词：

Euler parameters; Lie group; nonlinear H-infinity control; rigid body;

D O I：

10.1109/9.618253

中图分类号：

TP [自动化技术、计算机技术];

学科分类号：

0812 ;

摘要：

A state feedback H-infinity-suboptimal control problem on TSO(3) for a rigid spacecraft Kith three control torques and disturbances is addressed, The Hamilton-Jacobi inequality associated with a corresponding state feedback H-infinity-suboptimal control problem on TS3 is solved globally. The H-infinity-suboptimal state feedback on TS3 involves the Euler parameters and solves the original problem on TSO(3) when the initial values of the Euler parameters are appropriately chosen.

引用

页码：1186 / 1189

页数：4

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