Robust adaptive sliding mode attitude ...
Type de document :
Article dans une revue scientifique: Article original
URL permanente :
Titre :
Robust adaptive sliding mode attitude control for aircraft systems based on back-stepping method
Auteur(s) :
Zhuang, H. X. [Auteur]
Sun, Q. L. [Auteur]
Chen, Z. Q. [Auteur]
Zeng, Xianyi [Auteur]
Génie des Matériaux Textiles - ULR 2461 [GEMTEX]
École nationale supérieure des arts et industries textiles [ENSAIT]
Sun, Q. L. [Auteur]
Chen, Z. Q. [Auteur]
Zeng, Xianyi [Auteur]
Génie des Matériaux Textiles - ULR 2461 [GEMTEX]
École nationale supérieure des arts et industries textiles [ENSAIT]
Titre de la revue :
Aerospace Science and Technology
Nom court de la revue :
Aerosp. Sci. Technol.
Numéro :
118
Pagination :
-
Date de publication :
2021-10-07
ISSN :
1270-9638
Mot(s)-clé(s) en anglais :
Back-stepping method
Aircraft systems
Attitude control
Sliding mode control
Robust adaptive
Aircraft systems
Attitude control
Sliding mode control
Robust adaptive
Discipline(s) HAL :
Sciences de l'ingénieur [physics]
Résumé en anglais : [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, ...
Lire la suite >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.Lire moins >
Lire la suite >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.Lire moins >
Langue :
Anglais
Comité de lecture :
Oui
Audience :
Internationale
Vulgarisation :
Non
Établissement(s) :
Université de Lille
ENSAIT
Junia HEI
ENSAIT
Junia HEI
Collections :
Date de dépôt :
2023-06-20T11:55:27Z
2024-03-21T10:09:46Z
2024-03-21T10:09:46Z