1.
The Design of Attitude Control System of Moving Mass Actuated BTT Missile
变质心BTT拦截导弹姿态控制系统设计
2.
Terminal Sliding Mode Control for Attitude Control of Antiaircraft Missile
防空导弹姿态控制系统终态滑模变结构设计
3.
An Adaptive Attitude Control Law for Air-launched Cruise Missile
空射飞航导弹姿态控制的一种自适应方法
4.
Nonlinear Adaptive Control Theory with Applications to Missile Attitude Controller
非线性自适应控制理论在导弹姿态控制器设计中的应用
5.
Fuzzy Adaptive Variable Structure Control for Missile Attitude Control System Based on Improved Reaching Law
基于改进趋近律的模糊自适应滑模控制的导弹姿态控制系统
6.
Application of Ackermann Formula Based Discrete Grey Sliding Mode Control in Digital Missile Attitude Control System
基于Ackermann规则的离散全程灰色滑模控制在数字导弹姿态控制系统中的应用
7.
The Design of Terminal Sliding Control System for Vertical Launching Missile
垂直发射导弹Terminal滑模姿态控制系统设计
8.
Missile Attitude Tracking Robust Controller Design Under Parameter Uncertainty
参数不确定下导弹姿态跟踪鲁棒控制器设计
9.
Research on Robust and Adaptive Attitude Control System Design of Solid-propellant Ballistic Missile;
固体弹道导弹鲁棒及自适应姿态控制系统设计研究
10.
Lateral jet is an important means for missile control in high altitude.
侧向喷流是导弹在中高空进行姿态控制的重要手段。
11.
On attitude simulation of guided rocket projectiles with complete integrated GPS/INS navigation system
GPS/INS全组合制导火箭弹姿态仿真研究
12.
The Design of Differential Game Guidance Law Based on Target Attitude
基于目标姿态信息的导弹微分对策制导律研究
13.
Attitude Reference Design for Navigation and Control System of Underwater Carrier
水下载体导航控制系统姿态基准设计
14.
Variable Structure Control for the Attitude of Moving Mass Rotating Missile
旋转质量矩弹头双环滑模变结构姿态控制
15.
Control Attitude Angular Velocity for High-rolling Projectile by Moving-Mass Framework
滑块机构下高旋弹头的姿态角速度控制
16.
The Saturn guidance and control systems are designed to provide the proper trajectory and attitude orientation for the vehicle over a range of expected missions.
土星的导引和控制系统的设计能使飞行器在规定的任务范围内提供合适的弹道和姿态方位。
17.
The attitude control system of maneuver missile head is designed by applyi ng nonlinear decoupling control law.
然后采用非线性解耦控制理论设计了机动弹头的姿态控制系统。
18.
Dynamic Parameters Measurement and Attitude Simulation for the Cluster Fired by Combustion Gasbag
导弹囊抛子弹动态参数测试及姿态仿真研究