弹箭与制导学报
彈箭與製導學報
탄전여제도학보
JOURNAL OF PROJECTILES, ROCKETS, MISSILES AND GUIDANCE
2015年
1期
24-28
,共5页
高卫%孙奕帆%危艳玲
高衛%孫奕帆%危豔玲
고위%손혁범%위염령
电子对抗试验%导弹制导模拟%无人飞行器%飞行控制%导引律
電子對抗試驗%導彈製導模擬%無人飛行器%飛行控製%導引律
전자대항시험%도탄제도모의%무인비행기%비행공제%도인률
electronic warfare test%missile guidance simulation%unmanned aircraft%flight control%guidance law
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。
為瞭探索一種簡便經濟的導彈製導模擬方法以滿足電子對抗試驗需要,提齣瞭一種利用導引頭控製無人飛行器以模擬導彈製導過程的方法,利用電視導引頭搭載無人飛艇進行瞭飛行試驗驗證。基于飛艇飛控繫統縱嚮控製通道的分段式PID控製器以及特彆設計的製導指令生成模塊,利用電視導引頭測量的目標信息,分彆按照兩種導彈導引律控製和引導飛艇嚮目標飛行。對試驗結果的定量分析錶明,飛艇按照預設導引律成功實現瞭製導飛行。
위료탐색일충간편경제적도탄제도모의방법이만족전자대항시험수요,제출료일충이용도인두공제무인비행기이모의도탄제도과정적방법,이용전시도인두탑재무인비정진행료비행시험험증。기우비정비공계통종향공제통도적분단식PID공제기이급특별설계적제도지령생성모괴,이용전시도인두측량적목표신식,분별안조량충도탄도인률공제화인도비정향목표비행。대시험결과적정량분석표명,비정안조예설도인률성공실현료제도비행。
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.