the optimal guidance law 上述最优制导
LQG optimal guidance law LQG最优制导规律
optimal terminal guidance law 最优末制导律
optimal proportional guidance law 最优比例制导
an optimal terminal guidance law 离散时间最优末制导律
Simulation results indicate that the three guidance laws proposed are applicable to different cases, but compared with the classical optimal guidance law, the robustness is remarkably enhanced.
仿真结果表明,上述三种导引律各有适用范围,但与经典的最优导引律相比,鲁棒性均明显增强。
参考来源 - 天基对地打击武器轨道规划与制导技术研究·2,447,543篇论文数据，部分数据来源于NoteExpress
An optimal guidance law for reentry vehicle with high altitude maneuvering on downward phase is studied.
研究了在降弧段进行高空机动的再入飞行器最优制导律。
When targets fly with non-maneuvering, the optimal guidance law is the proportional guidance law with a changeable factor.
当目标作非机动飞行时，最优制导律是一种变比例系数的比例制导。
Furthermore, a guidance law is proposed by using a combination of optimal guidance law design with ideal velocity curve approach.
同时采用最优制导律设计与理想速度曲线相结合的方法，设计了能同时保证末端制导精度及速度方向、大小的制导律。
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