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题名: Visual simulation system design of soft-wing UAV based on FlightGear
作者: Qi JT(齐俊桐) ; Liu, Jinda ; Zhao BC(赵碧川) ; Mei S(梅森) ; Han JD(韩建达) ; Shang, Hong
作者部门: 机器人学研究室
会议名称: 11th IEEE International Conference on Mechatronics and Automation, IEEE ICMA 2014
会议日期: August 3-6, 2014
会议地点: Tianjin, China
会议录: 2014 IEEE International Conference on Mechatronics and Automation, IEEE ICMA 2014
会议录出版者: IEEE Computer Society
会议录出版地: Washington, DC
出版日期: 2014
页码: 1188-1192
收录类别: EI
ISBN号: 9781479939787
关键词: Aircraft ; Flexible structures ; Flight simulators ; Mathematical models
摘要: Soft-wing U AV is composed of soft ram air parafoil hanging powered vehicle with ropes. Benefit from its special mechanical structure and flight characteristics, soft-wing UAV has some advantages over other kinds of aircraft. However, because of these special characteristics make it possess apparent mass, flexible structure and relative motions between the parafoil and payload vehicle, which are the difficulties in research. Visual simulation based on mathematical model can vividly reappear the relationship between input and output of UAV and realize 3D visually simulation of the aircraft flight status. In this paper, based on the practical physical parameters of the self-designed soft-wing UAV, a 6 DOF mathematical model was built. Then a visual simulation system of soft-wing U AV based on FlightGear was designed. Finally, by using the simulation data from the soft-wing U AV mathematical model, the visual simulation was successfully realized. This visual simulation also testified the validation of this visual simulation system and mathematical model. © 2014 IEEE.
语种: 英语
产权排序: 1
内容类型: 会议论文
URI标识: http://ir.sia.cn/handle/173321/15158
Appears in Collections:机器人学研究室_会议论文

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Recommended Citation:
齐俊桐; Liu, Jinda; 赵碧川; 梅森; 韩建达; Shang, Hong.Visual simulation system design of soft-wing UAV based on FlightGear.见:IEEE Computer Society.2014 IEEE International Conference on Mechatronics and Automation, IEEE ICMA 2014,Washington, DC,2014,1188-1192
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