1.
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
2.
BTT Missile Autopilot Design Using Neural Networks;
基于神经网络的BTT导弹自动驾驶仪设计
3.
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
4.
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
5.
Nonlinear Missile Longitudinal Autopilot Design with Neural Net
非线性H_∞导弹纵向自动驾驶仪设计
6.
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
7.
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
8.
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
9.
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
10.
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
11.
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
12.
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
13.
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
14.
Missile H-infinity gain-scheduled autopilot design based on quasi-linear model
基于准线性化模型设计导弹H_∞增益调度自动驾驶仪
15.
Integral Fuzzy Sliding Mode Control for Missile Autopilot Design
积分模糊变结构控制的导弹侧向自动驾驶仪设计
16.
Design of air-to-air missile autopilot by nonlinear robust dynamic inversion
空空导弹鲁棒动态逆非线性驾驶仪设计
17.
In order to design the autopilot for a rear controlled missile we must make a first estimate of the required aerodynamic derivatives.
为了设计尾部控制导弹的自动驾驶仪，我们必须首先估算一下所需要的气动力导数。
18.
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