Trajectory tracking for mars atmospheric entry based on high-order sliding mode control

Juan Dai, Yuanqing Xia

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, the finite-time trajectory tracking control problem for Mars landing with disturbances is addressed. To improve the accuracy of Mars landing, a new nonlinear entry guidance law for low lift landers has been developed. The High-Order Sliding Mode Control(HOSMC) for a tracking a reference trajectory is proposed. The guidance method is based on HOSMC theory adapted to the problem of entry guidance. The HOSMC has been adapted to account for the specific 2-sliding modes exhibited by the longitudinal motion of the entry vehicle, using bank angle control for following a reference trajectory. The global stability nature of the HOSMC law is proven by using a Lyapunov-based approach. Extended state observer are applied to estimate the disturbance, by which sliding mode controllers are designed combing the two approaches respectively to force the state variables of the closed loop system to converge to the reference trajectory. Also, simulation results are presented to illustrate the effectiveness of the control strategy.

源语言英语
主期刊名Proceedings - 15th International Symposium on Parallel and Distributed Computing, ISPDC 2016
编辑Riqing Chen, Dan Grigoras, Chunming Rong
出版商Institute of Electrical and Electronics Engineers Inc.
395-400
页数6
ISBN(电子版)9781509041527
DOI
出版状态已出版 - 18 4月 2017
活动15th International Symposium on Parallel and Distributed Computing, ISPDC 2016 - Fuzhou, Fujian, 中国
期限: 8 7月 201610 7月 2016

出版系列

姓名Proceedings - 15th International Symposium on Parallel and Distributed Computing, ISPDC 2016

会议

会议15th International Symposium on Parallel and Distributed Computing, ISPDC 2016
国家/地区中国
Fuzhou, Fujian
时期8/07/1610/07/16

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