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巡航导弹末制导技术的发展
引用本文:廖朝佩. 巡航导弹末制导技术的发展[J]. 战术导弹技术, 1993, 0(3): 29-37
作者姓名:廖朝佩
作者单位:中国航天工业总公司三院
摘    要:简述了现有常规对陆攻击巡航导弹末制导系统,分析了它的缺陷和局限性。评述了未来巡航导弹末制导的发展趋向。指出成像早的是未来巡航导弹末制导的主要发展方向,为此需要在自动目标识别技术的开发方面做出努力。提出低速率修正末制导可作为自主寻的的一种替代办法。

关 键 词:巡航导弹  末制导  导引头  成像寻的

THE ADVANCE IN THE TERMINAL GUIDANCE TECHNOLOGY OF THE CRUISE MISSILES
Liao Chaopei The Third Research Academy of CASC. THE ADVANCE IN THE TERMINAL GUIDANCE TECHNOLOGY OF THE CRUISE MISSILES[J]. Tactical Missile Technology, 1993, 0(3): 29-37
Authors:Liao Chaopei The Third Research Academy of CASC
Affiliation:Liao Chaopei The Third Research Academy of CASC
Abstract:The current terminal guidance systems of the conventional land attack cruise missiles and its limitations are briefly described, the tendency of the development of tenninal guidance technology are reviewed, imaging homing guidance is primary direction of tenninal guidance of the future cruise missiles. However, it is necessary to make arduous efforts in the field of ATR Low update terminal guidance might be an altemative way of autonomous homing guidance.
Keywords:Cruise missile  Terminal guidance  Seeker  Imaging homing  
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