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科研机构
长春光学精密机械与物... [2]
内容类型
会议论文 [2]
发表日期
2011 [2]
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Establishment of airplane flight model and simulation analysis of landing behavior (EI CONFERENCE)
会议论文
2nd Annual Conference on Electrical and Control Engineering, ICECE 2011, September 16, 2011 - September 18, 2011, Yichang, China
Li M.
;
Li D.-W.
;
Jia H.-G.
;
Li L.
收藏
  |  
浏览/下载:17/0
  |  
提交时间:2013/03/25
This paper create a high fidelity plant model of an aircraft landing gear to inclusion into a full aircraft flight simulation for accurately analyzing the performance and influence of landing gear system. The use of domain specific modeling software enables detailed modeling of the physics and facilitates accurate computational simulation of the flight dynamic
aerodynamic
landing gear dynamic and mechanical loads that occur when the landing gear are deployed and retracted during landing and take-off operations. The parameter design space is easily searched by considering a number of different landing scenarios including touching down on one wheel first
to optimize the design. The simulation results show that the aircraft landing gear system mathematical model established appropriately reflects the change of force and moment in the process of taking off and landing
and it is actual in the physical process. 2011 IEEE.
Aircraft landing gear simulation using multidomain modeling technology (EI CONFERENCE)
会议论文
2011 International Conference on Information Technology, Computer Engineering and Management Sciences, ICM 2011, September 24, 2011 - September 25, 2011, Nanjing, Jiangsu, China
Li M.
;
Hao X.-Y.
;
Han X.-F.
;
Jia H.-G.
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  |  
浏览/下载:30/0
  |  
提交时间:2013/03/25
In order to accurately analyze the performance and influence of landing gear system
this paper presents a high fidelity plant model of an aircraft landing gear to inclusion into a full aircraft flight simulation. The use of domain specific modeling software enables detailed modeling of the physics and facilitates accurate computational simulation of the flight dynamic
aerodynamic
landing gear dynamic and mechanical loads that occur when the landing gear are deployed and retracted during landing and take-off operations. The parameter design space is easily searched by considering a number of different landing scenarios including touching down on one wheel first
to optimize the design. The simulation results show that the aircraft landing gear system mathematical model established appropriately reflects the change of force and moment in the process of taking off and landing
and it is improve the precision of flight simulation. 2011 IEEE.
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