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基于结构不确定性的非线性鲁棒制导律设计
引用本文:田宏亮,梁晓庚,贾晓洪,王鹏举.基于结构不确定性的非线性鲁棒制导律设计[J].飞行力学,2011,29(4):80-83.
作者姓名:田宏亮  梁晓庚  贾晓洪  王鹏举
作者单位:中国空空导弹研究院18所,河南洛阳,471009
摘    要:根据多普勒雷达导引头和红外成像导引头多模制导导弹弹道中段制导信息精度的特点,以非线性鲁棒控制理论为依据,设计了一种制导律.仿真结果表明,该制导律对弹目相对距离测量干扰有较好的鲁棒性,对目标大机动也有鲁棒性.因此,这种制导律可以作为多普勒雷达导引头和红外成像导引头多模制导导弹弹道中段的制导律使用.

关 键 词:飞行器控制、导航技术  非线性  鲁棒制导律  结构不确定性  多模制导

Design for nonlinear robust guidance law with structured uncertainties
TIAN Hong-liang,LIANG Xiao-geng,JIA Xiao-hong,WANG Peng-ju.Design for nonlinear robust guidance law with structured uncertainties[J].Flight Dynamics,2011,29(4):80-83.
Authors:TIAN Hong-liang  LIANG Xiao-geng  JIA Xiao-hong  WANG Peng-ju
Institution:TIAN Hong-liang,LIANG Xiao-geng,JIA Xiao-hong,WANG Peng-ju(The Eighteenth Department,China Airborne Missile Academy,Luoyang 471009,China)
Abstract:Based on the guidance information precision characteristic of the middle trajectory of multimode guidance missile with Doppler radar seeker and infrared imaging seeker,a guidance law was designed according to the nonlinear robust control theory.Simulation results show that the guidance law is robust to the measure disturbance of missile-target relative distance,and is also robust to a high maneuver target.So it can be used as the guidance law of the middle trajectory of multimode guidance missile with Doppl...
Keywords:aircraft control and navigation technologies  nonlinear  robust guidance law  structured uncertainty  multimode guidance  
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