Design of breakdown diagnose fuzzy - expert system for shore - to - ship missile automatic pilot 岸舰导弹自动驾驶仪故障诊断模糊专家系统设计
This thesis applies the robust h control theory to designing a btt missile ' s autopilot 本文利用鲁棒h _控制理论设计了高性能btt导弹自动驾驶仪。
This paper analyses the launching missiles stability of aircraft with an autopilot while launching 摘要对带有自动驾驶仪的飞机投弹时的稳定性进行了分析。
Finally , it has discussed how to establish the semi - physical simulation environment for digital autopilot system 最后论述了自动驾驶仪半物理仿真环境的建立。
On some missiles , these commands are generated internally by the missile computer autopilot 对于一些导弹而言，指令来自于内部，由弹载自动驾驶仪的计算机发出。
There are two mechanical pilots on the plane to take chage in case the human pilots cannot fly the plane 飞机上有两部机械自动驾驶仪，一旦驾驶员不能驾驶飞机时，它们能取代人操作。
The large airspace flying btt missile ' s autopilot is designed by using the robust h mixed sensitivity design method 应用鲁棒h _混合灵敏度设计方法设计了大空域btt导弹的自动驾驶仪。
The superbus would be driven in the usual way on roads and an autopilot would be engaged when it reached a supertrack 超级巴士能够行驶在普通的车道上，并且一旦接入超级车道自动驾驶仪就会开始工作。
Aiming at the anti - air missile flight control problem , a designing method of missile autopilot with fuzzy wavelet neural network is put forward 摘要针对防空导弹的飞行控制问题，提出一种基于模糊小波网络的导弹自动驾驶仪设计方法。
By the 3d simulation of the missile trajectory , the evaluation index , such as the kill probability , the hit precision can be obtained 建立了电视自动寻的制导导弹的完整模型，包括了传感器模型、过载控制模型、自动驾驶仪及导引头模型。
