Back-stepping Active Disturbance Rejection ...
Document type :
Article dans une revue scientifique: Article original
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Title :
Back-stepping Active Disturbance Rejection Control for Attitude Control of Aircraft Systems Based on Extended State Observer
Author(s) :
Zhuang, Huixuan [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]
Journal title :
International Journal of Control, Automation and Systems
Abbreviated title :
Int. J. Control Autom. Syst.
Volume number :
-
Pages :
-
Publication date :
2021-05-08
ISSN :
1598-6446
English keyword(s) :
Active disturbance rejection control
aircraft attitude control
back-stepping technique
extended state observer
aircraft attitude control
back-stepping technique
extended state observer
HAL domain(s) :
Sciences de l'ingénieur [physics]
English abstract : [en]
Robust flight control laws based on back-stepping technology and ADRC method are designed for attitude control of a non-linear aircraft system. First, non-linear aircraft model is introduced and converted to standard ...
Show more >Robust flight control laws based on back-stepping technology and ADRC method are designed for attitude control of a non-linear aircraft system. First, non-linear aircraft model is introduced and converted to standard equation of state. Then, the extended state observer is applied to estimate the unknown variables, the homologous ADRC is designed to ensure the state variables of the CLS to astringe to the reference state. Next, the stability of ESO and ADRC are analyzed and proven theoretically. At last, the effectiveness of this method is illustrated by extensive comparative simulations. The results acquired from simulation attest that ADRC can achieve better control performance than PID and SMC method.Show less >
Show more >Robust flight control laws based on back-stepping technology and ADRC method are designed for attitude control of a non-linear aircraft system. First, non-linear aircraft model is introduced and converted to standard equation of state. Then, the extended state observer is applied to estimate the unknown variables, the homologous ADRC is designed to ensure the state variables of the CLS to astringe to the reference state. Next, the stability of ESO and ADRC are analyzed and proven theoretically. At last, the effectiveness of this method is illustrated by extensive comparative simulations. The results acquired from simulation attest that ADRC can achieve better control performance than PID and SMC 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 :
2023-06-20T11:45:22Z
2024-03-21T08:17:04Z
2024-03-21T08:17:04Z
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