Active disturbance rejection based trajectory linearization control for hypersonic reentry vehicle with bounded uncertainties

被引:139
|
作者
Shao, Xingling [1 ,2 ]
Wang, Honglun [1 ,2 ]
机构
[1] Beijing Univ Aeronaut & Astronaut, Unmanned Aerial Vehicle Res Inst, Beijing 100191, Peoples R China
[2] Beijing Univ Aeronaut & Astronaut, Sci & Technol Aircraft Control Lab, Beijing 100191, Peoples R China
基金
中国国家自然科学基金;
关键词
Hypersonic reentry vehicle (HRV); Trajectory linearization control (TLC); Active disturbance rejection control (ADRC); Linear extended state observer (LESO); Actuator saturation; Feedback linearization; CONTROL DESIGN; OBSERVER;
D O I
10.1016/j.isatra.2014.06.010
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 investigates a novel compound control scheme combined with the advantages of trajectory linearization control (TLC) and alternative active disturbance rejection control (ADRC) for hypersonic reentry vehicle (HRV) attitude tracking system with bounded uncertainties. Firstly, in order to overcome actuator saturation problem, nonlinear tracking differentiator (TD) is applied in the attitude loop to achieve fewer control consumption. Then, linear extended state observers (LESO) are constructed to estimate the uncertainties acting on the LTV system in the attitude and angular rate loop. In addition, feedback linearization (FL) based controllers are designed using estimates of uncertainties generated by LESO in each loop, which enable the tracking error for closed-loop system in the presence of large uncertainties to converge to the residual set of the origin asymptotically. Finally, the compound controllers are derived by integrating with the nominal controller for open-loop nonlinear system and FL based controller. Also, comparisons and simulation results are presented to illustrate the effectiveness of the control strategy. (C) 2014 ISA. Published by Elsevier Ltd. All rights reserved.
引用
收藏
页码:27 / 38
页数:12
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