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基于Gauss伪谱法的空空导弹最优中制导律设计

杨希祥 张为华

国防科技大学学报2013,Vol.35Issue(1):28-32,5.
国防科技大学学报2013,Vol.35Issue(1):28-32,5.

基于Gauss伪谱法的空空导弹最优中制导律设计

Midcourse guidance law optimal design for air-to-air missiles based on gauss pseudospectral method

杨希祥 1张为华1

作者信息

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摘要

Abstract

The optimum design of midcourse guidance law for air-to-air missiles was researched based on Gauss Pseudospectral Method ( GPM) . The optimal control model for midcourse guidance law of air-to-air missiles was established, the idea to design optimal midcourse guidance law with GPM was proposed, the solving process was described in detail, and effectivity of the proposed method was verified with simulation cases. Simulation results show that GPM is dominant in performance index, computation accuracy and computation efficiency, compared with the traditional methods, such as proportional navigation and shooting method, and the computation accuracy and computation efficiency of GPM are determined by the number of collocation nodes. The above all can provide theoretical reference for research of midcourse guidance law for air-to-air missiles.

关键词

空空导弹/中制导律/最优控制/Gauss伪谱法

Key words

air-to-air missile/ midcourse guidance law/ optimal design/ Gauss Pseudospectral Method (GPM)

分类

军事科技

引用本文复制引用

杨希祥,张为华..基于Gauss伪谱法的空空导弹最优中制导律设计[J].国防科技大学学报,2013,35(1):28-32,5.

国防科技大学学报

OA北大核心CSCDCSTPCD

1001-2486

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