Accurate Homing of Parafoil Delivery Systems ...
Type de document :
Article dans une revue scientifique: Article original
URL permanente :
Titre :
Accurate Homing of Parafoil Delivery Systems Based Glide-Ratio Control
Auteur(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]
Titre de la revue :
IEEE Trans. Aerosp. Electron. Syst.
Nom court de la revue :
IEEE Trans. Aerosp. Electron. Syst.
Numéro :
56
Pagination :
2374-2389
Date de publication :
2020-07-16
ISSN :
0018-9251
Discipline(s) HAL :
Sciences de l'ingénieur [physics]
Résumé en anglais : [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 ...
Lire la suite >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.Lire moins >
Lire la suite >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.Lire moins >
Langue :
Anglais
Audience :
Internationale
Vulgarisation :
Non
Établissement(s) :
Université de Lille
ENSAIT
Junia HEI
ENSAIT
Junia HEI
Collections :
Date de dépôt :
2023-06-20T11:32:24Z
2024-01-31T10:53:41Z
2024-01-31T10:53:41Z