机动目标三维空间导引运动建模及导引律研究  

Modeling of Three-Dimensional Guidance Problems and Guidance Law Design against Maneuvering Targets

作　　者：张友安[1] 杨华东[1] 胡云安[1] 

机构地区：[1]海军航空工程学院301教研室,山东烟台264001

出　　处：《飞行力学》2003年第2期41-44,共4页Flight Dynamics

基　　金：航空科学基金资助项目 (99D1 2 0 0 1 )

摘　　要：给出了导弹 -目标追逃运动的空间矢量方程 ,在此基础上推导了三维导引运动模型。对机动目标应用李雅普诺夫稳定性分析方法提出了一种自适应变结构制导算法。Three dimensional vector equations for pursuit evasion motion of missile target are given. Dynamic equations for three dimensional guidance problems are derived. An adaptive variable structure guidance law against maneuvering targets is presented based on Lyapunov stability theory. 6DOF simulation results have shown the rightness of the model and the effectiveness of the proposed guidance law.

关 键 词：机动目标 导弹 自适应变结构控制 导引律 三维空间导引运动 数学建模 

分 类 号：TJ765[兵器科学与技术—武器系统与运用工程]