Sliding Mode Control for Mars Entry with Flatness and Extended State Observer

被引：0
|
作者：
Lu Kunfeng [1 ,2 ]
Xia Yuanqing [3 ]
Yu Chunmei [1 ,2 ,4 ]
Zhou Liuyu [5 ]
机构：
[1] Beijing Aerosp Automat Control Inst, Beijing 100854, Peoples R China
[2] Natl Key Lab Sci & Technol Aerosp Intelligent Con, Beijing 100854, Peoples R China
[3] Beijing Inst Technol, Sch Automat, Beijing 100081, Peoples R China
[4] Natl Univ Def Technol, Aerosp & Mat Engn, Changsha 410073, Hunan, Peoples R China
[5] Stanford Univ, Elect Engn, Stanford, CA 94305 USA
来源：
2015 34TH CHINESE CONTROL CONFERENCE (CCC) | 2015年
关键词：
Mars entry guidance and control; sliding mode control; Extended State Observer; Monte Carlo; GUIDANCE; TRACKING;
D O I：
暂无
中图分类号：
TP [自动化技术、计算机技术];
学科分类号：
0812 ;
摘要：
This paper addresses high-precision Mars entry guidance and control approach via sliding mode control (SMC) and Extended State Observer (ESO). First, differential flatness (DF) approach is applied to the dynamic equations of the entry vehicle. The presented control law requires no information on high uncertainties that are estimated by ESO. Finally, simulation results are presented to demonstrate the effectiveness of the proposed approach.
引用
收藏
页码：3275 / 3280
页数：6
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