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Sliding Mode Fault Tolerant Attitude Control Scheme for Spacecraft with Actuator Faults

CAO Teng GONG Huajun HAN Bing

南京航空航天大学学报（英文版）2019，Vol.36Issue(1)：119-127,9.

Sliding Mode Fault Tolerant Attitude Control Scheme for Spacecraft with Actuator Faults

CAO Teng ¹GONG Huajun ¹HAN Bing¹

作者信息

1. College of Automation Engineering,Nanjing University of Aeronautics and Astronautics,Nanjing 211106,P.R.China
折叠

摘要

关键词

fault tolerant control/fault estimation/actuator faults/sliding mode control

Key words

fault tolerant control/fault estimation/actuator faults/sliding mode control

分类

航空航天

引用本文复制引用

CAO Teng,GONG Huajun,HAN Bing..Sliding Mode Fault Tolerant Attitude Control Scheme for Spacecraft with Actuator Faults[J].南京航空航天大学学报（英文版）,2019,36(1):119-127,9.

基金项目

This work was partially supported by the National Natural Science Foundation of China(No. 61473143),Postgraduate Research & Practice Innovation Program of Jiangsu Province(No. KYCX18_0299),and the China Scholarships Council(No. 201806830102). （No. 61473143）

南京航空航天大学学报（英文版）

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ISSN：1005-1120

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