• Electronics Optics & Control
  • Vol. 21, Issue 9, 95 (2014)
KANG Zhiqiang, KOU Yingxin, LI Zhanwu, and CHEN Lei
Author Affiliations
  • [in Chinese]
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    DOI: 10.3969/j.issn.1671-637x.2014.09.021 Cite this Article
    KANG Zhiqiang, KOU Yingxin, LI Zhanwu, CHEN Lei. MidGuidance Instruction Calculation of Medium Range Air to Air Intercept Missile[J]. Electronics Optics & Control, 2014, 21(9): 95 Copy Citation Text show less

    Abstract

    The principle and the existing problems of radio amendment instruction consisted in the classical mediumrange airtoair intercept missile are described. Then a new method of variable period midguidance instruction is proposed. A variable period instruction model is established based on the Current Statistical Model (CSM) of target. The predicted target motion value is introduced into midguidance instruction,and the period of midguidance instruction is changed according to the estimated remaining time of midguidance. The simulation result indicates that the modified instruction model can improve the tracking efficiency of seeker and limit the error of targets designation angle in intercepting and capturing.
    KANG Zhiqiang, KOU Yingxin, LI Zhanwu, CHEN Lei. MidGuidance Instruction Calculation of Medium Range Air to Air Intercept Missile[J]. Electronics Optics & Control, 2014, 21(9): 95
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