【摘要】 针对导弹与目标之间的非线性运动学关系,在平行接近原理的基础上,结合轨迹线性化控制(TLC,trajectory linearization control)方法,为某型空-空导弹研究设计了一种新型的三维末制导律。仿真结果表明,所设计的基于TLC方法的制导律是有效的,且在目标机动情况下比传统的比例制导律以及滑模变结构制导律具有更好的制导性能。更多还原

【Abstract】 Aim at the nonlinear kinematics relation between the missile and target,based on the parallel approach principle,this paper studies and designs a novel three terminal guidance law.The simulating results show that the guidance law designed in this paper based on TLC method is effective and has better guidance performance than that of the conventional proportional and sliding model guidance law in the situation of target maneuver.更多还原