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作 者:谢晓阳[1] 洪东跑[1] 赵晓宁[1] 周国峰[1] Xie Xiao-yang;Hong Dong-pao;Zhao Xiao-ning;Zhou Guo-feng(China Academy of Launch Vehicle Technology, Beijing, 100076)
出 处:《导弹与航天运载技术》2017年第5期54-57,共4页Missiles and Space Vehicles
摘 要:针对机载导弹主被动雷达复合末制导系统的特点,在机载导弹典型实战任务剖面分析的基础上,综合考虑末制导主要性能参数、可靠性参数、实战环境条件等因素,建立基于ADC模型的复合末制导系统实战效能模型。通过对实战任务剖面下的主被动雷达复合末制导可用性、可信性和能力进行分析,实现对复合末制导系统实战效能的评估。以某机载导弹复合末制导系统为对象进行评估。结果表明,该模型综合考虑实战任务剖面、打击目标和实战环境,较好地满足了末制导作战效能评估的需求,可为机载导弹武器系统的效能评估提供有效支撑。According to the features of active-passive composite terminal guidance system and the operational pattern of airbornemissile,an operational effectiveness evaluation model was established to describe the influence of the performances of terminalguidance system,reliability index and battle circumstance on the operational effectiveness.Effectiveness of composite terminalguidance system can be evaluated by the analysis of availability,dependability and capability.The instance analysis shows that themodel is possible for engineering application.As the model reflects the real conditions of battle-field,it meets the requirements ofcomposite terminal guidance system evaluation,and provides support for effectiveness evaluation of airborne missile.
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