中国航天（英文版）2022，Vol.23Issue(2)：62-68,7.DOI:10.3969/j.issn.1671-0940.2022.02.008
Adaptive Reconfiguration for Launch Vehicle Under Servo Mechanism Fault
Adaptive Reconfiguration for Launch Vehicle Under Servo Mechanism Fault
HU Cunming 1ZHANG Weidong 2ZHOU Jing 1ZHANG Yifeng 1LI Guifang 1XU Xice3
作者信息
- 1. Shanghai Aerospace Control Technology Institute,Shanghai 201109
- 2. Shanghai Academy of Spaceflight Technology,Shanghai 201109
- 3. Nanjing University of Aeronautics and Astronautics,Nanjing 210016
- 折叠
摘要
关键词
launch vehicle/adaptive reconfiguration/pseudo-inverse method/linear programming/hybrid optimiza-tion method/SVDKey words
launch vehicle/adaptive reconfiguration/pseudo-inverse method/linear programming/hybrid optimiza-tion method/SVD引用本文复制引用
HU Cunming,ZHANG Weidong,ZHOU Jing,ZHANG Yifeng,LI Guifang,XU Xice..Adaptive Reconfiguration for Launch Vehicle Under Servo Mechanism Fault[J].中国航天（英文版）,2022,23(2):62-68,7.
