1.
Design of H_∞ Control Based Nonlinear Terminal Guidance Law
基于H_∞控制的非线性末制导律设计
2.
A Realizable Optimal Terminal Guidance Law
一种可实现的离散时间最优末制导律
3.
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
4.
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
5.
The Research of Missile Precision Terminal Guidance Law Based on Fuzzy Logic;
基于模糊逻辑的导弹精确末制导律研究
6.
Adaptive Terminal Sliding Mode Guidance Law for Air-to-Air Missile Based on Neural Network
空空导弹的神经网络自适应终端滑模末制导律
7.
Dynamic Inversion Based 3D Terminal Guidance Law Designed for Anti-Ship Cruise Missiles
基于动态逆的反舰巡航导弹三维末制导律设计
8.
Research on Terminal guidance law of missiles based on nonsingular terminal sliding mode
基于非奇异Terminal滑模的导弹末制导律研究
9.
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
10.
Design of a Variable Structure Terminal Guidance Law Based on Relative Velocity Deflection Angle
基于零化相对速度偏角的变结构末制导律设计
11.
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
12.
Research on 3D Terminal Guidance Laws Based on Actively Self-homing Spiral Variable Trajectory
基于主动螺旋变轨的三维末制导律研究
13.
Adaptive Terminal Guidance Law Based on Feedback Linearization for Maneuvering Targets
拦截机动目标自适应反馈线性化末制导律
14.
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
15.
Adaptive fuzzy guidance law for maneuvering targets
拦截机动目标的自适应模糊末制导律设计
16.
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
17.
Research on Cruise Missile s Three-Dimension Precise Terminal Guidance Law and 3D Animation Simulation;
巡航导弹的三维精确末制导律及三维动画仿真研究
18.
Terminal Guidance Law Design Based on Side Jet and Aerodynamic Compound Control;
基于直接侧向力/气动力复合控制的末制导律设计