A composite sliding mode control method for the design of missile roll autopilot is proposed.
针对导弹滚转驾驶仪模型,提出了一种复合滑模控制方案。
A Sliding mode control method for the design of roll autopilot was proposed.
提出了一种滑模变结构滚转驾驶仪的设计方法。
Research of Using Aerodynamic/Reaction-jet Controller for Designing Missile Autopilot;
气动力/直接力复合控制导弹自动驾驶仪设计研究
In this paper, the H∞ robust performance design method for the systems with mixed uncertainty is briefly introduced, and the problem of missile autopilot design is deeply studied.
简要介绍了复合摄动系统的H_∞鲁棒性能设计方法,并利用这种方法对导弹自动驾驶仪设计问题进行了研究。
Design of test system software for the missile autopilot
导弹自动驾驶仪测试系统软件的设计
The Autopilot Design for Axis-symmetrical Missile Based on Maneuvering Coordinates
基于机动坐标系的轴对称导弹自动驾驶仪设计
BTT Missile Autopilot Design Using Neural Networks;
基于神经网络的BTT导弹自动驾驶仪设计
Development of BTT Control Technique for Air-to-Air Missile Autopilot
空空导弹自动驾驶仪BTT控制算法发展综述
Research on autopilot of control system for portable antiaircraft missile
便携式防空导弹自动驾驶仪控制系统研究
Design and Simulation of Tactical Missile's Autopilot Based on Variable Structure Control
战术导弹自动驾驶仪变结构控制设计与仿真
The Design for Autopilot of Large Attack Angle Missile by Using Feedback Linearization Method
大攻角飞行导弹自动驾驶仪反馈线性化设计
Autopilot design for BTT missile based on fuzzy PID control
基于模糊PID控制的BTT导弹自动驾驶仪设计
Analysis for Control Method in Autopilot System of Aerodynamics Missile
飞航导弹自动驾驶仪系统控制方案研究
Three-Dimensional Nonlinear Guidance Law with Consideration of Autopilot Dynamics
考虑导弹自动驾驶仪动特性的三维非线性导引律
Design of Nonlinear Missile Autopilot Based on Robust Sliding Mode Control Method
基于鲁棒变结构控制方法的非线性导弹自动驾驶仪设计
Nonlinear Missile Longitudinal Autopilot Design with Neural Net
非线性H_∞导弹纵向自动驾驶仪设计
The Design of Autopilot for Bank-to-Turn Missile Based on Adaptive Neural Networks;
BTT导弹自适应神经网络自动驾驶仪设计
Robust Autopilot Desigh of BTT Missile Based on Composite Switching;
基于复合切换的BTT导弹鲁棒自动驾驶仪的设计
Design and Implementation of One Type of Bomb Autopilot Control System
某型制导炸弹自动驾驶仪控制系统设计与实现
Design of Optimal-Sliding Mode Nonlinear Autopilot for BTT Missile
BTT导弹非线性自动驾驶仪最优滑模设计
Comparison of Attitude and Overload Autopilots of Cruise Missile
巡航导弹姿态与过载自动驾驶仪对比研究
Missile gain-scheduled autopilot design using D-K-D iteration
采用D-K-D迭代算法设计导弹增益调度自动驾驶仪
