Study on System Design and Optimization for Guided Rockets Using Gauss Pseudospectral Method

  • YANG Jing ,
  • MAO Rui ,
  • DU Fenghuai ,
  • BAI Fengke ,
  • HUANG Ruochao
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  • Xi'an Modern Control Technology Research Institute, Xian 710065, China

Received date: 2018-01-10

  Online published: 2025-05-29

Abstract

Based on Gauss pseudospectral method, system design and optimization for guided rockets with impact-angle and terminal speed constraints was proposed. The trajectory optimization plan was established in which the target function was chosen as the speed at the impact point, and the impact angle as a terminal constraint. Numerical simulations were performed and the results show the speed profile of the guided rocket at impact point with respect to range. It is useful for guided rocket systems design in practice.

Cite this article

YANG Jing , MAO Rui , DU Fenghuai , BAI Fengke , HUANG Ruochao . Study on System Design and Optimization for Guided Rockets Using Gauss Pseudospectral Method[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2018 , 38(5) : 23 -26 . DOI: 10.15892/j.cnki.djzdxb.2018.05.006

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