空空导弹三维导引模型和机动目标导引规律研究  

Three-dimensional guidance model and law for air-to-air missile against maneuvering target

作　　者：张友安[1] 杨华东[1] 王士星[1] 

机构地区：[1]海军航空工程学院,山东烟台264001

出　　处：《现代防御技术》2003年第3期19-23,共5页Modern Defence Technology

基　　金：航空科学基金资助项目(No.99D12001)

摘　　要：给出了三维空间导弹-目标追逃运动的空间矢量方程,在三维空间建立了导弹-目标的追逃运动模型。在目标运动信息完全未知条件下对变速机动目标应用李雅普诺夫稳定性分析方法提出了一种非线性三维制导算法,这种方法在导引末段不需要过大的加速度命令,不需要知道目标精确的加速度和速度方位信息。全弹道六自由度数学仿真结果表明了模型的正确性和制导算法的有效性。The threedimensional vector equations for missiletarget pursuitevasion motion are given,the threedimensional pursuitevasion motion model is established,a threedimensional guidance algorithm is presented based on Lyapunov stability theory under the conditions that the accurate information of the target is unknown,exceed acceleration commands of missile in the final stage of the engagement and accurate information on the acceleration and velocity relative heading angle of the target in the proposed algorithm are not required.The rightness of the model and the effectiveness of the proposed arithmetic are showed by the 6DOF simulation. 

关 键 词：空空导弹 导引模型 机动目标导引规律 空间追逃问题 鲁棒制导 算法 全弹道仿真 

分 类 号：TJ762.23[兵器科学与技术—武器系统与运用工程] TJ765.3