A New Type of General Design Method for Median Guidance Law in Air-to-ground Missile Carried by Helicopter

MA Fei; YANG Kai; WANG Nizhi; WANG Lihao; XU Chen

doi:10.15892/j.cnki.djzdxb.2019.05.022

Journal of Projectiles, Rockets, Missiles and Guidance >

2019 , Vol. 39 >Issue 5: 95 - 98

DOI: https://doi.org/10.15892/j.cnki.djzdxb.2019.05.022

A New Type of General Design Method for Median Guidance Law in Air-to-ground Missile Carried by Helicopter

MA Fei ,
YANG Kai ,
WANG Nizhi ,
WANG Lihao ,
XU Chen

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Xi’an Modern Control Technology Research Institute, Xi’ an 710065, China

Received date: 2018-09-02

Online published: 2025-05-12

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Abstract

In view of the different launch altitude, different combat distance, different seeker’s capture field and the requirements of different attack modes of air-to-ground guided missiles, a new general design method of median guidance law is proposed to meet the various constraints at the same time in this paper.Mathematical simulation is adopted to verify the rationality and validity of the method.

Key words： air-to-ground guided missile; median guidance law; mathematical simulation

Cite this article

MA Fei , YANG Kai , WANG Nizhi , WANG Lihao , XU Chen . A New Type of General Design Method for Median Guidance Law in Air-to-ground Missile Carried by Helicopter[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2019 , 39(5) : 95 -98 . DOI: 10.15892/j.cnki.djzdxb.2019.05.022

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