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靶弹平飞高度拓展的设计与实现

王刚 张驰 吴建业

舰船电子工程2017,Vol.37Issue(2):38-41,4.
舰船电子工程2017,Vol.37Issue(2):38-41,4.DOI:10.3969/j.issn.1672-9730.2017.02.010

靶弹平飞高度拓展的设计与实现

Design and Realization of Target Missile Trajectory Height Expansion

王刚 1张驰 1吴建业1

作者信息

  • 1. 91851部队 葫芦岛 125001
  • 折叠

摘要

Abstract

In this paper, a lot of measures are used for the sea skimming flight target missile flying at a height of 1000 meters, such as adding missile used digital computer, replacing new type radio altimeter and changing control channel parameter.This target missile is used to simulate airplane.The stable flight influenced by noise increased above 1000 metres result from the new type radio altimeter is solved by changing the PID control parameter, inertia time constant and differential calculating step.In the end, the methed of the target missile modifying for flying at 1000 meters is proved correct by mathematical simulation.

关键词

靶弹/高度表/PID

Key words

target missile/altimeter/PID

分类

航空航天

引用本文复制引用

王刚,张驰,吴建业..靶弹平飞高度拓展的设计与实现[J].舰船电子工程,2017,37(2):38-41,4.

舰船电子工程

OACSTPCD

1672-9730

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