2) velocity pursuit guidance law
速度追踪制导律
1.
Taking initial aiming error as inertial small perturbance,we established a model of guidance loop with velocity pursuit guidance law at the ideal conditions and deduced an analytical expression.
以导弹初始瞄准误差为初始小扰动,建立理想条件下速度追踪制导律制导回路模型,在此基础上求解其解析表达式。
2.
This paper describes the basic principle of velocity pursuit guidance law and body pursuit guidance law of trajectory correction projectiles, researches the terminal correction trajectory and miss distance under pursuit guidance laws by 6—DOF trajectory simulation program, researches the orbit of laser detector ray axis and ground projection area of laser detector spatial viewpoint.
文中对速度追踪制导律和弹体追踪制导律的工作原理进行了研究,利用六自由度弹道仿真程序对弹道修正弹两种追踪方式下的末段修正弹道和脱靶量进行了对比计算,研究了两种追踪方式下激光探测器光轴的轨迹及激光探测器空间视场在地面投影区域的变化;弹体追踪方式命中精度虽然较低,但由于工程实现简单、成本低,仍有其工程使用价值。
3) Import tracking system
进口追踪制度
4) Velocity Pursuit
速度追踪
1.
Modeling and Analysis of the Guidance Loop for the Missile Velocity Pursuit Guidance Law;
速度追踪制导律导引回路建模及解析分析
5) Angular Trackong
角度追踪
6) traitor tracing scheme
追踪体制
1.
This paper proposed a new discrete logarithm based public key traitor tracing scheme.
给出了一个新的基于离散对数的公钥追踪体制。
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