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应用动态逆理论的反舰导弹规避机动导引律设计
引用本文:范作娥,马培蓓,顾文锦.应用动态逆理论的反舰导弹规避机动导引律设计[J].东南大学学报(自然科学版),2011,41(Z1):64-67.
作者姓名:范作娥  马培蓓  顾文锦
作者单位:1. 海军航空工程学院控制工程系,烟台,264001
2. 海军航空工程学院指挥系,烟台,264001
基金项目:航空科学基金和航空电子系统综合技术国防科技重点实验室联合资助项目(20095584006)
摘    要:为了提高反舰导弹的突防能力,有效规避敌方舰空导弹的拦截,完成精确打击目标的战术要求,从便于工程实现的角度出发,应用时标分离的方法,将弹目相对运动模型分离为2个一阶的动力学子系统,这2个子系统分别对应于视线角速率层(慢动力学系统)和自动驾驶仪惯性滞后层(快动力学系统),对这2个子系统分别进行动态逆控制设计,设计了一种能够...

关 键 词:导引律  反舰导弹  动态逆  规避机动

Evasive maneuver guidance law design using dynamic inversion for anti-ship missile
Fan Zuoe,Ma Peibei,Gu Wenjin.Evasive maneuver guidance law design using dynamic inversion for anti-ship missile[J].Journal of Southeast University(Natural Science Edition),2011,41(Z1):64-67.
Authors:Fan Zuoe  Ma Peibei  Gu Wenjin
Institution:Fan Zuoe1 Ma Peibei2 Gu Wenjin1 (1Department of Control Engineering,Naval Aeronautical and Astronautical University,Yantai 264001,China) (2Department of Commanding,China)
Abstract:In order to improve the survivability of anti-ship missile against anti-air missile,and achieve the tactical mission of accurately attacking the target,based on the time-scale separation the relative motion model of missile and target was separated into two subsystems: the angular rate of line-of-sight subsystem(the low speed subsystem),and the autopilot lag subsystem(the fast speed subsystem).Dynamic inversion controllers were designed for the two subsystems respectively.The dynamic inversion guidance law ...
Keywords:guidance law  anti-ship missile  dynamic inversion  evasive maneuver    
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