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Volume 39 Issue 5
May  2013
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Journal of Beijing University of Aeronautics and Astronautics  > 2013  >  39(5): 580-584.
Jia Zhongren, Huang Chengtao, Wang Lixinet al. Mathematical simulation method to calculate air minimum control speed[J]. Journal of Beijing University of Aeronautics and Astronautics, 2013, 39(5): 580-584. (in Chinese)
Citation: Jia Zhongren, Huang Chengtao, Wang Lixinet al. Mathematical simulation method to calculate air minimum control speed[J]. Journal of Beijing University of Aeronautics and Astronautics, 2013, 39(5): 580-584. (in Chinese)
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Mathematical simulation method to calculate air minimum control speed

  • School of Aeronautic Science and Engineering, Beijing University of Aeronautics and Astronautics, Beijing 100191, China

  • Received Date: 10 May 2012
  • Rev Recd Date: 26 Nov 2012
  • Publish Date: 31 May 2013
    Abstract
  • The determination of the air minimum control speed VMC is an important content in the civil aircraft airworthiness compliance verification. The value of VMC is one of the vital bases to design the rudder and engine layout of an aircraft. Based on the physical understanding of the VMC airworthiness compliance flight test, a method to calculate VMC by mathematical simulation was proposed. According to the behavior characteristics of the pilot in the VMC flight test, the mathematical pilot model was established. Then, the pilot-aircraft closed loop flight simulation model for the VMC flight test was set up. Based on the accurate mathematical simulation of the VMC flight test, the value of VMC under different test conditions can be obtained. The method to calculate VMC proposed has important theoretical and practical value to guide the aircraft design and airworthiness compliance flight test.

     

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