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- self adaptive flight control system 自适应飞行控制系统
- ADAPTIVE FLIGHT CONTROL SYSTEM OF ARMED HELICOPTER USING WAVELET NEURAL NETWORK METHOD 神经网络自适应控制在攻击直升机中的应用
- Adaptive Flight Control System of Air to Air Missile with Quantitative Feedback Theory 空空导弹自适应飞控系统的定量反馈理论设计
- The Study of Self - Adaptive Flight Control System for Aircraft With Thrust Vector and Simulation Platform 推力矢量飞机自适应控制系统仿真平台研究
- The Design for a New Adaptive Flight Control System of Maneuvering Entry Aerospacecraft 机动再入飞行器自适应飞行控制系统设计
- The Design and Simulation Study of Missile Adaptive Flight Control System 自适应制导控制系统的设计与仿真研究
- Adaptive Flight Control System 自适应飞行控制系统
- Subsystems of flight control system II. 飞行控制系统的分系统2。
- Reconfigurable Direct Adaptive Flight Control System Based on RBF Neural Network 具有重构功能的基于RBF神经网络直接自适应飞控系统
- JOHNSON E N, KANNAN S. Adaptive flight control for an autonomous unmanned helicopter [R]. AIAA Paper: AIAA - 2002 - 4439. 徐锦法.;无人飞行器分布式控制系统集成新技术[J]
- To overcome the disadvantage of the traditional gain scheduling method in flight control system design, a model reference adaptive backstepping PID control scheme is proposed. 为克服飞行控制系统设计中传统增益规划方案的缺点,提出一类飞机纵向运动模型参考反推自适应PID控制方案,并给出了该方案的具体设计过程和跟踪性能改善方法。
- The design of the flight control system with the vectored thrust is discussed. 对带推力矢量飞机的飞控设计问题进行了研究。
- And during this case, flight control system (FCS) plays a more important role . 在上述改进的基础上,飞行控制系统起到关键性的作用。
- Missile rudders are executive bodies of missile flight control system. 舵机测试系统是导弹生产线上的重要设备。
- ALTITUDE ACQUIRE, A digital flight control system mode to transition from climb (or descend) to level flight. 高度截获,一种数字式飞行操纵系统,从爬升(或下降)改平的模式。
- That defect could cause solders to crack and the flight control system to fail, Ernst explains. 他拒绝提供细节,他的观点是,假零件肯定会导致严重事故。
- A new approach based on LPV model to design large envelope flight control system is presented. 介绍一种基于线性参变模型(LPV)设计大包线飞行控制器的新方法。
- Abstract: The design of the flight control system with the vectored thrust is discussed. 文摘:对带推力矢量飞机的飞控设计问题进行了研究。
- Abstract: The design of the flight control system with the vectored thrust is discussed. 摘 要: 对带推力矢量飞机的飞控设计问题进行了研究。
- The research emphasis of flight control system of UAH is to determine the flight states of UAH by use of measured data. 利用有限的测量数据来确定无人直升机的飞行状态变量是无人直升机飞行控制系统研究的热点。