利用导引头控制无人飞行器模拟导弹制导过程的试验研究

高卫; 孙奕帆; 危艳玲

doi:10.15892/j.cnki.djzdxb.2015.01.007

弹箭与制导学报 >

2015 , Vol. 35 >Issue 1: 24 - 28

DOI: https://doi.org/10.15892/j.cnki.djzdxb.2015.01.007

导弹与制导技术

利用导引头控制无人飞行器模拟导弹制导过程的试验研究

高卫 ,
孙奕帆 ,
危艳玲

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1 北京跟踪与通信技术研究所,北京 100094
2 北京航天飞行控制中心,北京 102206

高卫(1970-),男,陕西榆林人,博士,研究员,研究方向:电子对抗试验技术。

收稿日期: 2014-03-12

网络出版日期: 2025-05-26

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The Method for Simulating Missile Guidance Process with the Unmanned Aircraft Piloted by a Homing Seeker

GAO Wei ,
SUN Yifan ,
WEI Yanling

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1 Beijing Institute of Tracking and Telecommunications Technology, Beijing 100094, China
2 Beijing Aerospace Control Center, Beijing 102206, China

Received date: 2014-03-12

Online published: 2025-05-26

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摘要

为了探索一种简便经济的导弹制导模拟方法以满足电子对抗试验需要,提出了一种利用导引头控制无人飞行器以模拟导弹制导过程的方法,利用电视导引头搭载无人飞艇进行了飞行试验验证。基于飞艇飞控系统纵向控制通道的分段式PID控制器以及特别设计的制导指令生成模块,利用电视导引头测量的目标信息,分别按照两种导弹导引律控制和引导飞艇向目标飞行。对试验结果的定量分析表明,飞艇按照预设导引律成功实现了制导飞行。

关键词： 电子对抗试验; 导弹制导模拟; 无人飞行器; 飞行控制; 导引律

本文引用格式

高卫 , 孙奕帆 , 危艳玲 . 利用导引头控制无人飞行器模拟导弹制导过程的试验研究[J]. 弹箭与制导学报, 2015 , 35(1) : 24 -28 . DOI: 10.15892/j.cnki.djzdxb.2015.01.007

Abstract

In order to explore a simple and convenient method for simulating missile guidance to meet the need in electronic warfare test, a method for simulating missile guidance process with the unmanned aircraft piloted by a homing seeker is put forward and validated by flight test with an unmanned airship loaded with a TV seeker. Based on the segmented PID controller of the longitudinal control channel of the airship flight control system and the guidance command creator specially designed for the test, an airship is piloted by the target information produced by a TV seeker loaded on the airship towards the target according to two guidance laws respectively. The test results show that the airship realizes guidance flight successfully according to the preset guidance laws.

Key words： electronic warfare test; missile guidance simulation; unmanned aircraft; flight control; guidance law

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参考文献

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