midcourse guidance meaning in Chinese
飞行中段引导
中程制导
Examples
- Study of handing over between midcourse guidance and terminal guidance for multi - purpose missiles
多用途导弹中末段交班研究 - The proposed algorithm can be used in the design of pure inertial midcourse guidance scheme
该算法可用于纯惯性中制导方案设计。 - The simulation result shows that the influence of the midcourse guidance based on the inertial navigation on the missile ' s impact point is remarkable
仿真结果表明，纯惯导中制导对洲际导弹落点精度影响比较大。 - Forth , this thesis also had made a preliminary discussion on the integrated guidance system of air - to - air missile beyond visual range air combat and made deep research on the midcourse guidance stage , thus we obtained an extremely useful conclusion .
本文还对空空导弹超视距攻击的复合制导体制做了一个初步的探讨,并对其中的中制导阶段进行了深入研究,得到了一个十分有用的结论:即中制导阶段导弹发动机的最优推力方向实际上应该是关于时间的线性函数。 - Based on optimal control theory and singularly perturbed theory , a singularly perturbed midcourse guidance law that guarantees air - to - ground missiles to ascent quickly is proposed . this new guidance law is a composite control law consisting of three parts : optimal climbing control using variable weighting factor method , minimum energy cruising phase control and minimum energy switching phase control . moreover , a new control logic is designed in order to remove influence of climbing control on switching phase . simulation results of a certain type of air - to - ground missile are presents . it is shown that , with simple control algorithm and feasible onboard implementation , this law not only guarantees air - to - ground missiles to ascent quickly , but also satisfies the requirements of midcourse phases . the studies have important theoretical meaning and great value of engineering application
为满足实际作战的要求，基于最优控制理论和奇异摄动方法，提出了一种可保证中远程空地导弹快速爬升到最优高度的中制导律.它由变系数最优爬升控制，最小能量巡航控制和最小能量下滑控制组成.为了减小爬升段控制对下滑段的影响，提出了一种新的控制逻辑.最后针对某型空地导弹进行了仿真.结果表明，该中制导律较好地满足了中远程空地导弹在中制导段的要求.本文的研究结果具有较好地工程参考价值