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《Transactions of Beijing Institute of Technology》 2019-08
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Research on ADRC-Based Trajectory Linearization Control of Hypersonic Reentry Vehicle

ZHANG Hui-ping;YU Yue;WANG Hong-lun;School of Automation, Beijing Institute of Technology;Beijing Aerospace Automatic Control Institute;School of Automation Science and Electrical Engineering, Beihang University;Science and Technology Laboratory on Aircraft Control,Beihang University;  
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.
【Fund】: 航空科学基金资助项目(2014ZA51002)
【CateGory Index】: V448;TJ765
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【Citations】
Chinese Journal Full-text Database 1 Hits
1 Jie Wang*,Qun Zong,Bailing Tian,and Helong LiuSchool of Electrical Engineering and Automation,Tianjin University,Tianjin 300072,China;Flight control for a flexible air-breathing hypersonic vehicle based on quasi-continuous high-order sliding mode[J];Journal of Systems Engineering and Electronics;2013-02
【Co-citations】
Chinese Journal Full-text Database 7 Hits
1 Xiang-yu ZHANG;Guo-hong WANG;Zhen-yu SONG;Jiao-jiao GU;Institute of Information Fusion,NAAU;Department of Scientific ResearchNAAU;;Hypersonic sliding target tracking in near space[J];Defence Technology;2015-04
2 ZHANG Xiang-yu;WANG Guo-hong;ZHANG Jing;LIU Yuan;Institute of Information Fusion of Naval Aeronautical and Astronautical University;;Tracking of Hypersonic Boost-to-Glide Trajectory Target in Near-Space[J];宇航学报;2015-10
3 ZHANG Xiangyu;WANG Guohong;LI Junjie;SHENG Dan;Institute of Information Fusion,Naval Aeronautical and Astronautical University;;Tracking of hypersonic sliding target in near-space[J];航空学报;2015-06
4 BU Xiangwei;WU Xiaoyan;CHEN Yongxing;ZHANG Rui;Air and Missile Defense College,Air Force Engineering University;;Adaptive backstepping control of hypersonic vehicles based on nonlinear disturbance observer[J];国防科技大学学报;2014-05
5 Liang Wang;Yongzhi Sheng;Xiangdong Liu;School of Automation,Beijing Institute of Technology;Key Laboratory for Intelligent Control & Decision of Complex Systems,Beijing Institute of Technology;;High-order sliding mode attitude controller design for reentry flight[J];Journal of Systems Engineering and Electronics;2014-05
6 Zong Qun;Su Rui;Wang Jie;Tian Bailing;School of Electrical Engineering and Automation,Tianjin University;;Adaptive High-Order Terminal Sliding Mode Control for Hypersonic Flight Vehicle[J];天津大学学报(自然科学与工程技术版);2014-11
7 HOU De-long;WANG Qing;DONG Chao-yang;HUANG Xi-yuan;Science and Technology on Aircraft Control Laboratory,Beihang University;School of Aeronautic Science and Engineering,Beihang University;Research and Development Center,China Academy of Launch Vehicle Technology;;Adaptive tracking control for switched polytopic system of hypersonic vehicle[J];系统工程与电子技术;2014-05
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