吉林大学学报(工学版) ›› 2011, Vol. 41 ›› Issue (增刊2): 241-245.

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Dynamics modeling and simulation of helicopter aviation

LI Ying-jie1,2, ZHAO Ding-xuan1, ZHAO Ying1, HOU Jing-wei1, LI Shan-feng3, YANG Guo-jun2   

  1. 1. College of Mechanical Science and Engineering, Jilin University, Changchun 130022, China;
    2. Base of Foundation, Aviation University of Air Force, Changchun 130022, China;
    3. Jilin Railway Vocational Technology College, Jilin 132002, China
  • Received:2010-12-30 Online:2011-09-30 Published:2011-09-30

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Abstract:

In order to achieve the aim of virtually piloting on flight simulator,6-DOF dynamics model of helicopter was established.Based on Lagrange equation,taking the real-timely acquired state information from joystick as the input,a simplified analytical model for the force on helicopter was proposed.Adopting Runge-Kutta iterative arithmetic,the dynamics equation was solved in real time.Finally,the higher reliability of the model and simulation algorithm was verified through comparing with actual flight data and simulation scene,so it can be seen as a more accurate research in advance for helicopter maneuver flight subject.

Key words: applied mechanics, dynamics model, Lagrange equation, simulation, helicopter

CLC Number: 

  • O313.3


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