Robust adaptive sliding mode attitude ...
Document type :
Article dans une revue scientifique: Article original
Permalink :
Title :
Robust adaptive sliding mode attitude control for aircraft 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 :
Aerospace Science and Technology
Abbreviated title :
Aerosp. Sci. Technol.
Volume number :
118
Pages :
-
Publication date :
2021-10-07
ISSN :
1270-9638
English keyword(s) :
Back-stepping method
Aircraft systems
Attitude control
Sliding mode control
Robust adaptive
Aircraft systems
Attitude control
Sliding mode control
Robust adaptive
HAL domain(s) :
Sciences de l'ingénieur [physics]
English abstract : [en]
In this paper, the robust adaptive control and back-stepping method are considered for attitude control of aircraft systems. First, a non-linear aircraft model is introduced and converted to standard state space form. Then, ...
Show more >In this paper, the robust adaptive control and back-stepping method are considered for attitude control of aircraft systems. First, a non-linear aircraft model is introduced and converted to standard state space form. Then, an adaptive sliding mode controller is designed by using the back-stepping method. An adaptive law is designed to cooperate with sliding mode control (SMC) to compensate for the unknown and uncertain parts of the aircraft systems. This method does not need to know the physical parameters of the aircraft model accurately, but only uses the adaptive upper bound of the matrix model norm to ensure the robustness of the system under SMC. Next, the stability of the adaptive law and SMC is analyzed and proven theoretically. At last, the effectiveness of this method is illustrated by extensive comparative simulations. Furthermore, the disturbance term is introduced to test the anti-interference performance of the controller. The results acquired from simulation illustrate that SMC can achieve good control performance.Show less >
Show more >In this paper, the robust adaptive control and back-stepping method are considered for attitude control of aircraft systems. First, a non-linear aircraft model is introduced and converted to standard state space form. Then, an adaptive sliding mode controller is designed by using the back-stepping method. An adaptive law is designed to cooperate with sliding mode control (SMC) to compensate for the unknown and uncertain parts of the aircraft systems. This method does not need to know the physical parameters of the aircraft model accurately, but only uses the adaptive upper bound of the matrix model norm to ensure the robustness of the system under SMC. Next, the stability of the adaptive law and SMC is analyzed and proven theoretically. At last, the effectiveness of this method is illustrated by extensive comparative simulations. Furthermore, the disturbance term is introduced to test the anti-interference performance of the controller. The results acquired from simulation illustrate that SMC can achieve good control performance.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 :
2023-06-20T11:55:27Z
2024-03-21T10:09:46Z
2024-03-21T10:09:46Z