Active disturbance rejection control for drag tracking in mars entry guidance

被引：76
作者：
Xia, Yuanqing [1 ]
Chen, Rongfang [1 ]
Pu, Fan [1 ]
Dai, Li [1 ]
机构：
[1] Beijing Inst Technol, Sch Automat, Beijing 100081, Peoples R China
来源：
ADVANCES IN SPACE RESEARCH | 2014年 / 53卷 / 05期
基金：
中国国家自然科学基金;
关键词：
Precision landing capability; Closed-loop guidance schemes; ADRC; Monte Carlo; QUATERNION BASED CONTROL; ADAPTIVE TRACKING;
D O I：
10.1016/j.asr.2013.12.008
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
Future Mars missions will require precision landing capability, which motivates the need for entry closed-loop guidance schemes. A new tracking law - active disturbance rejection control (ADRC) - is presented in this paper. The ability of the ADRC tracking law to handle the atmospheric models and the vehicle's aerodynamic errors is investigated. Monte Carlo simulations with dispersions in entry state variables, drag and lift coefficients, and atmospheric density show effectiveness of the proposed algorithm. (C) 2013 COSPAR. Published by Elsevier Ltd. All rights reserved.
引用
收藏
页码：853 / 861
页数：9
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