弹道学报Issue(4)：1-6,6.
推力矢量拦截弹制导控制一体化设计
Integrated Guidance and Control of Interceptor With Thrust Vector Control
摘要
Abstract
Aiming at interceptor with thrust vector control,a method for integrated guidance and control was proposed.Based on the introduction of equivalent elevator angle,multiple-inputs control problem was transformed into a single input problem,and the problem of normalizing the thrust vector and aerodynamic force was resolved.The strategy of control distribution was designed,and expressions of elevator angle and thrust vector deflection angle were given.On the basis of the simplified and standardized model of attack-defense confrontation,integrated guidance and control law was obtained by using backstepping method and Lyapunov redesign method. Numerical simulation results show that the interceptors with this law of integrated guidance and control cannot only get targets effectively,but also make attitudes and the angles of actuators change smoothly compared with conventional method of guidance law and control law designed respectively.关键词
拦截弹/推力矢量/控制分配/制导控制一体化/反步法Key words
interceptor/thrust vector control/control distribution/integrated guidance and control/backstepping分类
航空航天引用本文复制引用
惠耀洛,南英,邹杰..推力矢量拦截弹制导控制一体化设计[J].弹道学报,2015,(4):1-6,6.基金项目
航空科学基金项目(20140152002) （20140152002）
南京航空航天大学研究生创新基地(实验室)开放基金(kfjj201458) （实验室）
中央高校基本科研业务费专项基金项目 （）
