Magnetic Attitude Control of Bias Momentum Spacecraft by Bounded Linear Feedback

被引：0
|
作者：
Luo, Weiwei [1 ]
Zhou, Bin [1 ]
机构：
[1] Harbin Inst Technol, Ctr Control Theory & Guidance Technol, Harbin 150001, Heilongjiang, Peoples R China
来源：
2017 29TH CHINESE CONTROL AND DECISION CONFERENCE (CCDC) | 2017年
基金：
中国国家自然科学基金;
关键词：
Attitude stabilization; Lyapunov stable; Lyapunov equation; Magnetic torque; Bounded feedback; SATELLITES; SATURATION; ACTUATION; SYSTEMS;
D O I：
暂无
中图分类号：
TP [自动化技术、计算机技术];
学科分类号：
0812 ;
摘要：
This paper addresses the three-axis magnetic attitude control of small spacecraft with momentum bias configuration by bounded linear feedback. Necessary and sufficient conditions are derived to guarantee that the linearized dynamics and kinematics are stable in the Lyapunov sense. Explicit solutions to some Lyapunov equations associated with the considered open-loop system are obtained. Based on the explicit solutions to the Lyapunov equation, an explicit saturated linear state feedback controller is designed. Globally asymptotic stability of the closed-loop systems is proved by constructing the explicit Lyapunov function. Simulations show the effectiveness of the proposed approach.
引用
收藏
页码：3933 / 3938
页数：6
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