Accurate Homing of Parafoil Delivery Systems ...
Document type :
Article dans une revue scientifique: Article original
Permalink :
Title :
Accurate Homing of Parafoil Delivery Systems Based Glide-Ratio Control
Author(s) :
Sun, Hao [Auteur]
Sun, Qinglin [Auteur]
Zeng, Xianyi [Auteur]
Ecole nationale supérieure des arts et industries textiles de Roubaix (ENSAIT)
Luo, Shuzhen [Auteur]
Wu, Wannan [Auteur]
Chen, Zengqiang [Auteur]
Sun, Qinglin [Auteur]
Zeng, Xianyi [Auteur]
Ecole nationale supérieure des arts et industries textiles de Roubaix (ENSAIT)
Luo, Shuzhen [Auteur]
Wu, Wannan [Auteur]
Chen, Zengqiang [Auteur]
Journal title :
IEEE Trans. Aerosp. Electron. Syst.
Abbreviated title :
IEEE Trans. Aerosp. Electron. Syst.
Volume number :
56
Pages :
2374-2389
Publication date :
2020-07-16
ISSN :
0018-9251
HAL domain(s) :
Sciences de l'ingénieur [physics]
English abstract : [en]
In this article, the proposed method first evaluates the effects on aerodynamic force caused by flight velocity and angular velocity of the parafoil delivery system and performs an active disturbance rejection control in ...
Show more >In this article, the proposed method first evaluates the effects on aerodynamic force caused by flight velocity and angular velocity of the parafoil delivery system and performs an active disturbance rejection control in the horizontal direction. Moreover, a glide-ratio controller is designed based on the characteristics of the symmetrical flap deflection. For resisting its disturbance, a feedforward compensation unit is designed with the glide-ratio controller. The performance is effectively validated through hardware-in-the-loop simulation.Show less >
Show more >In this article, the proposed method first evaluates the effects on aerodynamic force caused by flight velocity and angular velocity of the parafoil delivery system and performs an active disturbance rejection control in the horizontal direction. Moreover, a glide-ratio controller is designed based on the characteristics of the symmetrical flap deflection. For resisting its disturbance, a feedforward compensation unit is designed with the glide-ratio controller. The performance is effectively validated through hardware-in-the-loop simulation.Show less >
Language :
Anglais
Audience :
Internationale
Popular science :
Non
Administrative institution(s) :
Université de Lille
ENSAIT
Junia HEI
ENSAIT
Junia HEI
Collections :
Submission date :
2023-06-20T11:32:24Z
2024-01-31T10:53:41Z
2024-01-31T10:53:41Z