Aerodynamic surfaces control allocation for RLV reentry

Zhi Xu, Shuo Tang

科研成果: 书/报告/会议事项章节会议稿件同行评审

3 引用 (Scopus)

摘要

In this paper, aerodynamic control surfaces of reusable launch vehicle (RLV) in reentry phase were converted into a constrained optimization problem, and using a mixed linear programming algorithm to solve them. For nonlinear between aerodynamic control surfaces and control torque, the piecewise linear programming algorithm was used to solve the control surfaces failure and on-line reconfigurable optimization problem. Finally, simulation verify three failure modes of aerodynamic surfaces by piecewise linear programming method and aerodynamic surfaces can be reconstructed with good performance and a smaller allocation error.

源语言英语
主期刊名Proceedings - 2010 2nd International Conference on Intelligent Human-Machine Systems and Cybernetics, IHMSC 2010
73-76
页数4
DOI
出版状态已出版 - 2010
活动2010 2nd International Conference on Intelligent Human-Machine Systems and Cybernetics, IHMSC 2010 - Nanjing, 中国
期限: 26 8月 201028 8月 2010

出版系列

姓名Proceedings - 2010 2nd International Conference on Intelligent Human-Machine Systems and Cybernetics, IHMSC 2010
1

会议

会议2010 2nd International Conference on Intelligent Human-Machine Systems and Cybernetics, IHMSC 2010
国家/地区中国
Nanjing
时期26/08/1028/08/10

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