跳到主要导航 跳到搜索 跳到主要内容

Fault tolerant attitude tracking control for Mars entry vehicles via Takagi-Sugeno model

科研成果: 书/报告/会议事项章节会议稿件同行评审

摘要

In this paper, a fault tolerant fuzzy tracking controller is designed for Mars entry vehicles during the entry phase in the presence of actuator failures. The original nonlinear attitude dynamics are divided into two subsystems based on the concept of time-scale decomposition. Dynamic inversion method is employed for the slow kinematic subsystem to give the angular velocity command by taking the attitude command as its input. The Takagi-Sugeno (T-S) fuzzy model based control method is applied for the fast kinetic subsystem by taking angular velocity command as its input to derive the desired control torque in the presence of actuator failures. Finally, the simulation results are given to demonstrate the effectiveness of the developed method for the Mars entry fault tolerant attitude control problem.

源语言英语
主期刊名2014 IEEE Chinese Guidance, Navigation and Control Conference, CGNCC 2014
出版商Institute of Electrical and Electronics Engineers Inc.
2299-2304
页数6
ISBN(电子版)9781479946990
DOI
出版状态已出版 - 12 1月 2015
活动6th IEEE Chinese Guidance, Navigation and Control Conference, CGNCC 2014 - Yantai, 中国
期限: 8 8月 201410 8月 2014

出版系列

姓名2014 IEEE Chinese Guidance, Navigation and Control Conference, CGNCC 2014

会议

会议6th IEEE Chinese Guidance, Navigation and Control Conference, CGNCC 2014
国家/地区中国
Yantai
时期8/08/1410/08/14

指纹

探究 'Fault tolerant attitude tracking control for Mars entry vehicles via Takagi-Sugeno model' 的科研主题。它们共同构成独一无二的指纹。

引用此