1.
A Realizable Optimal Terminal Guidance Law
一种可实现的离散时间最优末制导律
2.
An Optimal Terminal Guidance Based on Schwartz Inequality
一种基于许瓦兹不等式的最优末制导律设计
3.
Study on the Optimal Terminal Guidance Law with Interception and Impact Angle
带落点和落角约束的最优末制导律研究
4.
Trajectory Simulations on Active-Radar-Guided AAM Based on Optimal Guidance Law
基于最优末制导律的主动雷达空空导弹的弹道研究
5.
Optimal Terminal Missile Guidance Law Based on Fuzzy Neural Networks
基于模糊神经网络的导弹最优寻的末制导律
6.
An Optimal Space Terminal Guidance Law Based on Inverse System
一种基于逆系统方法的最优空间末制导律
7.
A RANDOM OPTIMAL GUIDANCE LAW OF AIR-TO-AIR MISSILE IN ALL DIRECTIONS
空-空导弹全向攻击随机最优制导律
8.
Application of LQG Optimal Guidance Law to Ground-to-air Missile
LQG最优制导规律在地空导弹中的应用
9.
An Optimal Guidance Law Based on Zero Miss-distance
一种基于零脱靶量的最优制导律设计
10.
The Use of Steepest Ascent Method in Optimal Guidance Law Simulation of Missile
梯度法在导弹最优制导律仿真中的应用
11.
Design and Simulation of Handover Performance Optimal Midcourse Guidance Law
一种交班时刻性能最优的中制导律设计与仿真
12.
An Optimal Guidance Law for Reentry Warhead Base on Angular Velocity
一种基于角速率的再入弹头最优制导律
13.
Research on Optimal Sliding-Mode Guidance Law Based on Hopfield Neural Network
基于Hopfield神经网络的最优滑模制导律研究
14.
Performance of proportional navigation law for terminal laserguided projectile
激光末制导炮弹比例导引律性能研究
15.
Design of H_∞ Control Based Nonlinear Terminal Guidance Law
基于H_∞控制的非线性末制导律设计
16.
Optimum Design of Variable Structure Guidance Law for Exoatmospheric Endgame Interception
大气层外末段拦截变结构制导律设计
17.
A terminal guidance law design applied to space-to-surface precision attack weapons
天对地精确攻击武器末段制导律设计
18.
Deep space impact exploration guidance based on advanced predictive guidance
基于改进预测制导的深空撞击探测末制导律