...
机译:具有较大冲击角约束和时差估计的有偏差比例导航制导律
Department of Control Engineering, Naval Aeronautical and Astronautical University, ErMa Road No. 188, ZhiFu District, Yantai, China;
Department of Control Engineering, Naval Aeronautical and Astronautical University, Yantai, China,Unit 93132, PLA, Qiqihar, China;
Department of Control Engineering, Naval Aeronautical and Astronautical University, Yantai, China;
Guidance law; biased proportional navigation guidance; impact angle control; impact time control; time-to-go estimation;
机译:比例导航制导的准确时间估计
机译:具有冲击角约束的走时加权最优制导
机译:没有寻求走时信息的考虑搜寻者视场约束的影响时间控制制导律
机译:具有精确冲击角的走时有理函数偏差PN引导律
机译:使用理想比例导航制导的用于移动物体拦截的工业机器人系统。
机译:游击猎鹰的终末攻击轨迹由导弹的比例导航制导定律描述
机译:近距离接近阶段的偏差比例导航制导律