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近距引导战斗机自动攻击控制律实现

陈中起 张斌 杜永伟 冯国强

火力与指挥控制2012,Vol.37Issue(5):148-151,155,5.
火力与指挥控制2012,Vol.37Issue(5):148-151,155,5.

近距引导战斗机自动攻击控制律实现

The Realization of Auto Attack Control Law for Short-distance Guidance of Fighter Plane

陈中起 1张斌 1杜永伟 1冯国强1

作者信息

  • 1. 空军工程大学工程学院,西安 710038
  • 折叠

摘要

Abstract

In accordance with the short-distance guidance procedure for modern fighter plane to target airspace, firstly, the relative moving model of fighter plane and target is built, then, the auto-attack conception is put forward, and a kind of auto-attack guidance law of fighter plane based on sight error is given. Based on those, auto attack control law is designed. At last a simulation example is given whose results show that this method works perfectly to eliminate aiming error, and it is suitable for the auto-attack of aircraft.

关键词

近距引导/瞄准误差/自动攻击/控制律

Key words

short-distance guidance/ sight error/ auto-attack/ rule of control

分类

航空航天

引用本文复制引用

陈中起,张斌,杜永伟,冯国强..近距引导战斗机自动攻击控制律实现[J].火力与指挥控制,2012,37(5):148-151,155,5.

基金项目

航空科学基金资助项目(20095196012) (20095196012)

火力与指挥控制

OA北大核心CSCDCSTPCD

1002-0640

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