机译:高攻角导弹的滚-俯仰-偏航集成μ综合
School of Mechanical & Aerospace Engineering, Seoul National University, Seoul, Republic of Korea;
School of Mechanical & Aerospace Engineering, Seoul National University, Seoul, Republic of Korea;
School of Mechanical & Aerospace Engineering, Seoul National University, Seoul, Republic of Korea,Defence Development (ADD 09-01-03-03) and Institute of Advanced Aerospace Technology at Seoul National University;
Guidance and Control Directorate, Agency for Defense Development, Daejeon, Republic of Korea;
Guidance and Control Directorate, Agency for Defense Development, Daejeon, Republic of Korea;
Division of Aerospace Engineering, Korea Advanced Institute of Science and Technology, Daejeon, Republic of Korea;
Radar R&D Center, Samsung Thales Co., Yongin, Republic of Korea;
robust control; μ synthesis; aerodynamic coupling; multivariable system; skid-to-turn missile;
机译:高攻角导弹的滚动俯仰偏航集成鲁棒自动驾驶仪设计
机译:高攻角导弹的滚动俯仰偏航集成鲁棒自动驾驶仪设计
机译:基于局部状态观测器的全局快速终端滑模控制的非线性时变导弹横滚偏航自动驾驶仪设计
机译:强大的滚动间距偏移为高角度导弹综合自动扫描
机译:导弹拦截器集成指导和控制:单环高阶滑动模式方法
机译:基于SINS / CNS深度集成模式的弹道导弹导航系统最大熵无味卡尔曼滤波。
机译:基于局部状态观测器的全局快速终端滑模控制的非线性时变导弹横滚偏航自动驾驶仪设计
机译:冲压发动机导弹综合飞控/燃油控制系统的综合。