Research on ADRC-Based Trajectory Linearization Control of Hypersonic Reentry Vehicle

被引：0
|
作者：
Zhang H.-P. [1 ,2 ]
Yu Y. [3 ,4 ]
Wang H.-L. [3 ,4 ]
机构：
[1] School of Automation, Beijing Institute of Technology, Beijing
[2] Beijing Aerospace Automatic Control Institute, Beijing
[3] School of Automation Science and Electrical Engineering, Beihang University, Beijing
[4] Science and Technology Laboratory on Aircraft Control, Beihang University, Beijing
来源：
Beijing Ligong Daxue Xuebao/Transaction of Beijing Institute of Technology | 2019年 / 39卷 / 08期
关键词：
Active disturbance rejection control; Decoupling control; Hypersonic reentry vehicle; Trajectory linearization control;
D O I：
10.15918/j.tbit1001-0645.2019.08.013
中图分类号：
学科分类号：
摘要：
Based on the kinematic model of hypersonic reentry vehicle, coupling effects between three channels were comprehensively analyzed, including kinematics coupling, inertial coupling, aerodynamic coupling and control coupling. To solve the attitude tracking problem of the strong coupling system, ADRC(active disturbance rejection control)-based trajectory linearization controllers were designed based on time-scale separation and singular perturbation theory for attitude and angular rate loops respectively. During design process, decoupling mechanism of ADRC-based trajectory linearization control were analyzed fully from perspective of feedforward, feedback, disturbance estimation and compensation. The simulation results show the correctness of the decoupling mechanism analysis and excellent decoupling effects of ADRC-based trajectory linearization control possesses, being suited to design controller for strong coupling systems. © 2019, Editorial Department of Transaction of Beijing Institute of Technology. All right reserved.
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页码：852 / 858
页数：6
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