Controllability of Spacecraft Attitude and Its Application in Reconfigurability Analysis

被引：0

作者：

Yang H. ^{[1
]}

Meng Q. ^{[1
]}

Jiang B. ^{[1
]}

机构：

[1] College of Automation Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing

来源：

Transactions of Nanjing University of Aeronautics and Astronautics | 2019年 / 36卷 / 02期

基金：

中国国家自然科学基金;

关键词：

Controllability; Fault tolerant control; Geometry control theory; Spacecraft attitude control;

D O I：

10.16356/j.1005-1120.2019.02.001

中图分类号：

学科分类号：

摘要：

We review the controllability research on spacecraft attitude based on nonlinear geometry control theory. The existing studies on attitude controllability are mostly concerning the global controllability and small time local controllability (STLC). A presentation of study methods and connotation in both aspects is briefly carried out. As a necessary condition of reconfigurability, the controllability of the faulty attitude control system is studied. Moreover, two reconfigurability conditions based on controllability results that consider the actuator faults for a pyramid configuration spacecraft are provided. © 2019, Editorial Department of Transactions of NUAA. All right reserved.

引用

页码：189 / 196

页数：7

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