Active Disturbance Rejection Control for ...
Document type :
Article dans une revue scientifique: Article original
Permalink :
Title :
Active Disturbance Rejection Control for Attitude Control of Missile Systems Based on Back-stepping Method
Author(s) :
Zhuang, H. X. [Auteur]
Sun, Q. L. [Auteur]
Chen, Z. Q. [Auteur]
Zeng, Xianyi [Auteur]
École nationale supérieure des arts et industries textiles [ENSAIT]
Génie des Matériaux Textiles - ULR 2461 [GEMTEX]
Sun, Q. L. [Auteur]
Chen, Z. Q. [Auteur]
Zeng, Xianyi [Auteur]
École nationale supérieure des arts et industries textiles [ENSAIT]
Génie des Matériaux Textiles - ULR 2461 [GEMTEX]
Journal title :
International Journal of Control, Automation and Systems
Abbreviated title :
Int. J. Control Autom. Syst.
Volume number :
-
Pages :
-
Publication date :
2021-09-13
ISSN :
1598-6446
English keyword(s) :
Back-stepping technique
linear active disturbance rejection control
linear extended state observer
missile attitude control
linear active disturbance rejection control
linear extended state observer
missile attitude control
HAL domain(s) :
Sciences de l'ingénieur [physics]
English abstract : [en]
In this paper, a novel attitude control method for nonlinear missile system is proposed, which combines backstepping technique with linear active disturbance rejection control (LADRC). Firstly, the nonlinear missile model ...
Show more >In this paper, a novel attitude control method for nonlinear missile system is proposed, which combines backstepping technique with linear active disturbance rejection control (LADRC). Firstly, the nonlinear missile model is introduced and transformed into the standard state equation. The linear extended state observer (LESO) is used to estimate the unknown variables. Compared with PID control method, the homologous LADRC design ensures that the state variables of the closed-loop system converge to the reference state. The stability of LESO and LADRC is theoretically analyzed and proved. A large number of comparative simulations show the effectiveness of the method. The simulation results show that LADRC has better control performance than SMC and PID method.Show less >
Show more >In this paper, a novel attitude control method for nonlinear missile system is proposed, which combines backstepping technique with linear active disturbance rejection control (LADRC). Firstly, the nonlinear missile model is introduced and transformed into the standard state equation. The linear extended state observer (LESO) is used to estimate the unknown variables. Compared with PID control method, the homologous LADRC design ensures that the state variables of the closed-loop system converge to the reference state. The stability of LESO and LADRC is theoretically analyzed and proved. A large number of comparative simulations show the effectiveness of the method. The simulation results show that LADRC has better control performance than SMC and PID method.Show less >
Language :
Anglais
Peer reviewed article :
Oui
Audience :
Internationale
Popular science :
Non
Administrative institution(s) :
Université de Lille
ENSAIT
Junia HEI
ENSAIT
Junia HEI
Collections :
Submission date :
2023-06-20T11:54:23Z
2024-03-21T10:02:13Z
2024-03-21T10:02:13Z
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