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Volume 40 Issue 3
Mar.  2014
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Journal of Beijing University of Aeronautics and Astronautics  > 2014  >  40(3): 370-376.
Diao Xinghua, Fang Yangwang, Wu Youli, et al. Simulation analysis on air-to-air missile allowable launch envelope about cooperative air combat of multi-fighter formation[J]. Journal of Beijing University of Aeronautics and Astronautics, 2014, 40(3): 370-376. doi: 10.13700/j.bh.1001-5965.2013.0237(in Chinese)
Citation: Diao Xinghua, Fang Yangwang, Wu Youli, et al. Simulation analysis on air-to-air missile allowable launch envelope about cooperative air combat of multi-fighter formation[J]. Journal of Beijing University of Aeronautics and Astronautics, 2014, 40(3): 370-376. doi: 10.13700/j.bh.1001-5965.2013.0237(in Chinese)
shu

Simulation analysis on air-to-air missile allowable launch envelope about cooperative air combat of multi-fighter formation

doi: 10.13700/j.bh.1001-5965.2013.0237
  • 1.

    Aeronautics and Astronautics Engineering College, Air Force Engineering University, Xi'an 710038, China

  • 2. Unit 94676 of People's Liberation Army, Shanghai 202178, China

  • Received Date: 02 May 2013
  • Publish Date: 20 Mar 2014
    Abstract
  • A method for calculating allowable launch envelope of air-to-air missile in multi-aircraft cooperative air warfare was researched. The mechanism of launch envelope of air-to-air missile was analyzed of single-aircraft in the actual case. Considering the mode of cooperative launch/guidance of air-to-air missile, the definition of cooperative launch envelope was conclude. Based on the target, missile and aircraft movement model and the constraints of cooperative launch envelope, the golden section-probability searching method was proposed to calculate the cooperative launch envelope, and some simulations were made to work out the parameters' affection in case of two fighters cooperatively attacking. Simulation results show that multi-aircraft cooperative guidance can enlarge the allowable launch envelope of missile obviously and the cooperative launch envelope was affected by the parameters of the guider and the missile.

     

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