In this paper,an optimal guidance law for missiles with impact angle and miss distance constraints is proposed to achieve the maximal terminal velocity. The normal acceleration command that includes the timevarying co...In this paper,an optimal guidance law for missiles with impact angle and miss distance constraints is proposed to achieve the maximal terminal velocity. The normal acceleration command that includes the timevarying coefficients is introduced to satisfy the desired impact angle as well as zero miss distance according to the geometric relation and relative motion parameters between missile and target. The problem is formulated as an optimal control problem by defining the angle of velocity error and flight-path angle as state variables and maximizing a performance index of the terminal velocity. The analytical form of the proposed guidance law is obtained as the solution of the optimal control problem combining optimal control theory and numerical value computation method. Nonlinear simulations of various situations demonstrate the performance and feasibility of the proposed optimal guidance law.展开更多
针对杆式爆炸成型侵彻体(Explosively formed penetrator, EFP)的侵彻能力问题,利用数值仿真手段开展杆式EFP侵彻特性研究,分析杆式EFP成型形态、着靶速度及材料特性对其侵彻能力的影响,得到杆式EFP成型特征参数在侵彻过程中的影响规律...针对杆式爆炸成型侵彻体(Explosively formed penetrator, EFP)的侵彻能力问题,利用数值仿真手段开展杆式EFP侵彻特性研究,分析杆式EFP成型形态、着靶速度及材料特性对其侵彻能力的影响,得到杆式EFP成型特征参数在侵彻过程中的影响规律。研究结果表明:杆式EFP在侵彻过程中,除初始阶段(碰撞后)和最后阶段(杆侵蚀后)外,弹体保持恒定速度运动,满足恒速杆假设;稳定侵彻时,随着密实部长度的逐渐减小,中空尾裙部材料不断流入密实部补充其侵蚀损失。增加弹体长度可以在一定程度上提高EFP的侵彻能力,但归一化侵彻深度下降;提高着靶速度和密实部长度可以显著提升杆式EFP侵彻性能。杆式EFP的强度对侵彻的影响有限,但靶体强度不可忽略,弹靶材料密度是影响侵彻体侵彻的主要因素。展开更多
基金Sponsored by the National Security Academic Foundation(Grant No.11176012)the CALT University Joint innovation Foundation(Grant No.CALT 201302)
文摘In this paper,an optimal guidance law for missiles with impact angle and miss distance constraints is proposed to achieve the maximal terminal velocity. The normal acceleration command that includes the timevarying coefficients is introduced to satisfy the desired impact angle as well as zero miss distance according to the geometric relation and relative motion parameters between missile and target. The problem is formulated as an optimal control problem by defining the angle of velocity error and flight-path angle as state variables and maximizing a performance index of the terminal velocity. The analytical form of the proposed guidance law is obtained as the solution of the optimal control problem combining optimal control theory and numerical value computation method. Nonlinear simulations of various situations demonstrate the performance and feasibility of the proposed optimal guidance law.
文摘针对杆式爆炸成型侵彻体(Explosively formed penetrator, EFP)的侵彻能力问题,利用数值仿真手段开展杆式EFP侵彻特性研究,分析杆式EFP成型形态、着靶速度及材料特性对其侵彻能力的影响,得到杆式EFP成型特征参数在侵彻过程中的影响规律。研究结果表明:杆式EFP在侵彻过程中,除初始阶段(碰撞后)和最后阶段(杆侵蚀后)外,弹体保持恒定速度运动,满足恒速杆假设;稳定侵彻时,随着密实部长度的逐渐减小,中空尾裙部材料不断流入密实部补充其侵蚀损失。增加弹体长度可以在一定程度上提高EFP的侵彻能力,但归一化侵彻深度下降;提高着靶速度和密实部长度可以显著提升杆式EFP侵彻性能。杆式EFP的强度对侵彻的影响有限,但靶体强度不可忽略,弹靶材料密度是影响侵彻体侵彻的主要因素。
