A FIXED-TIME TERMINAL SLIDING-MODE CONTROL FOR MARS ENTRY VEHICLE

被引：0
|
作者：
Wei Haogong [1 ]
Wang Qiang [1 ]
机构：
[1] Beijing Inst Spacecraft Syst Engn, Beijing 100094, Peoples R China
来源：
FOURTH IAA CONFERENCE ON DYNAMICS AND CONTROL OF SPACE SYSTEMS 2018, PTS I-III | 2018年 / 165卷
关键词：
D O I：
暂无
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
This paper presents a novel fixed-time terminal sliding -mode control (TSMC) for Mars entry vehicle with system uncertainties and external perturbations. A newly defined non-singular terminal sliding surface is constructed and a guaranteed closed -loop convergence time independent of initial states is derived based on the phase plane analysis and Lyapunov tools. The performance of the guidance methodology is verified by simulations of a Mars entry vehicle in the end.
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页码：521 / 529
页数：9
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