Nonlinear attitude state tracking control for spacecraft

被引：105
作者：
Xing, GQ [1 ]
Parvez, SA [1 ]
机构：
[1] Space Prod & Applicat Inc, Fairfax, VA 22030 USA
来源：
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS | 2001年 / 24卷 / 03期
关键词：
D O I：
10.2514/2.4754
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
Two attitude state controllers are designed for tracking of large-angle manewvers by applying a set of relative attitude kinematics and dynamics equation, where the attitude is represented by the relative modified Rodrigues parameters. Using such equations to design tracking controller converts the tracking control problem into a regulator problem and simplifies the design procedure.
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页码：624 / 626
页数：3
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