Modeling of powered parafoil based on Kirchhoff motion equation

被引：82
|
作者：
Zhu, Erlin [1 ]
Sun, Qinglin [1 ]
Tan, Panlong [1 ]
Chen, Zengqiang [1 ]
Kang, Xiaofeng [2 ]
He, Yingping [3 ]
机构：
[1] Nankai Univ, Coll Comp & Control Engn, Tianjin 300071, Peoples R China
[2] Aerosp Life Support Ind Ltd, Mil Representat Off, Xiangyang 441003, Peoples R China
[3] AVIC Aerosp Life Support Ind Ltd, Xiangyang 441003, Peoples R China
来源：
NONLINEAR DYNAMICS | 2015年 / 79卷 / 01期
基金：
中国国家自然科学基金;
关键词：
Powered parafoil; Relative motion; Dynamic model; Kirchhoff motion equation;
D O I：
10.1007/s11071-014-1690-9
中图分类号：
TH [机械、仪表工业];
学科分类号：
0802 ;
摘要：
Powered parafoil is a kind of flexible wing vehicle, which is composed of traditional parafoil system and power plant. Considering the relative motion of canopy and payload, two coordinates are built separately to analyze the motion properties of canopy and payload. According to the Kirchhoff motion equation, eight degrees of freedom (DOF) dynamic model of powered parafoil is built, including six DOF motion of canopy and relative yaw and relative pitch motion of payload. The simulation focuses on the basic motions of gliding, turning, flare landing and the responses to the wind and power. The simulation results verify the validity of dynamic model of powered parafoil.
引用
收藏
页码：617 / 629
页数：13
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