A Trajectory Optimization Method for Hypersonic Gliding Missile

LIU Zhongxin; MIAO Haochun; HUANGFU Yilun; LI Yajun; GAO Dengwei; FU Bo

doi:10.15892/j.cnki.djzdxb.2024.03.005

Journal of Projectiles, Rockets, Missiles and Guidance >

2024 , Vol. 44 >Issue 3: 35 - 42

DOI: https://doi.org/10.15892/j.cnki.djzdxb.2024.03.005

A Trajectory Optimization Method for Hypersonic Gliding Missile

LIU Zhongxin ,
MIAO Haochun ,
HUANGFU Yilun ,
LI Yajun ,
GAO Dengwei ,
FU Bo

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

Received date: 2023-10-17

Online published: 2024-12-28

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Abstract

In this paper, a trajectory optimization method of hypersonic glide missile is put forward by using penalty function method to hand non full course flying height and angle of attack constraints, which is based on Gauss Pseudo-spectral Method and takes into account multi phases, multi complex constraints and penetration mission-oriented requirements and so on. Its simulation results show that all constraint indexes are effectively controlled, and the penalty function method has more advantages in handling mission segmented constraints compared to conventional segmented constraint methods, which verified the effective coverage ability of the method under different ranges, launch heights and target heights.

Key words： Gauss pseudo-spectral method; performance index; penalty function; trajectory optimization

Cite this article

LIU Zhongxin , MIAO Haochun , HUANGFU Yilun , LI Yajun , GAO Dengwei , FU Bo . A Trajectory Optimization Method for Hypersonic Gliding Missile[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2024 , 44(3) : 35 -42 . DOI: 10.15892/j.cnki.djzdxb.2024.03.005

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