1) initial guidance
初制导
1.
In this paper,the precise initial guidance law based on velocity gain guidance and the state transition matrix for orbit interception were proposed.
对于轨道拦截问题,给出了一种基于速度增益制导和状态转移矩阵的精确初制导方法。
2.
The Lambert interception based on the two-body theory can be used to design the initial guidance for an exoatmospheric fixed-time interception.
仿真结果表明,该摄动修正方法合理、有效,可以在只增加较少燃料消耗的情况下,快速进行初制导修正,大大提高远距离拦截的制导精度。
2) initial guidance law
初制导律
1.
A closed-form initial guidance law based on feed forward and feedback neural network control for finite propulsive reentry spacecraft was presented.
提出了一种前馈反馈神经网络闭路初制导律。
2.
Based on analysis of characteristics of initial guidance, a new initial guidance law and a new method of calculating time to go are brought forward.
在分析组合制导中初制导阶段特点的基础上 ,给出了一种新的初制导律形式 ,并且提出了一种适合初制导律的剩余时间拟合方法。
4) Pilot Study of Tutorial System for the Undergraduates
初探本科生导师制
5) Exploration into Dormitory Students Tutorial System
住宿生导师制初探
补充资料：波束制导(见遥控制导)
波束制导(见遥控制导)
beam-rider guidance
boshu zhidao波束制导(beam一rider guidanee)见遥控制导。
说明：补充资料仅用于学习参考，请勿用于其它任何用途。
参考词条