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Journal of Projectiles, Rockets, Missiles and Guidance >

2021 , Vol. 41 >Issue 3: 81 - 83

DOI: https://doi.org/10.15892/j.cnki.djzdxb.2021.03.017

A General Design Method for Pitch Attitude Scheme of Air-to-ground Missile Carried by Helicopter

  • MA Fei ,
  • YANG Kai ,
  • XU Chen ,
  • HE Yi ,
  • WANG Nizhi
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  • Xi’an Modern Control Technology Research Institute,Xi’an 710065, China

Received date: 2020-07-18

  Online published: 2025-02-20

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Abstract

In view of the characteristic that the launch altitude of air-to-ground guided missiles carried by helicopter varies in a certain range, considering median guidance law, a new general design method for pitch attitude scheme of air-to-ground missile carried by helicopter is proposed.The method is adopted by designing a set of control meter and interpolation scheme for pitch attitude scheme to solve the problem that traditional design method can not adapt to the challenges for the launch envelope of air-to-ground missile carried by helicopter. Mathematical simulation is adopted to verify the rationality and validity of the method.

Key words： air-to-ground missile; pitch attitude scheme; mathematical simulation

Cite this article

MA Fei , YANG Kai , XU Chen , HE Yi , WANG Nizhi . A General Design Method for Pitch Attitude Scheme of Air-to-ground Missile Carried by Helicopter[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2021 , 41(3) : 81 -83 . DOI: 10.15892/j.cnki.djzdxb.2021.03.017

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