| 1. | 4 . robust control methods of ema are studied
研究了电动舵机的h _鲁棒控制方法。 |
| 2. | Segment sliding mode control of missile ' s electromechanical actuation
导弹电动舵机系统的分段滑模控制 |
| 3. | A research and design of entire dual redundancy electro - mechanical actuator
完全双余度电动舵机系统的研究与设计 |
| 4. | Analysis of the feasibility and reliability of electromechanical actuator for btt missile
导弹电动舵机系统的可行性与可靠性分析 |
| 5. | 2 . mathematical models of the ema activated by pmsm and latm are established
建立了基于pmsm及latm不同驱动类型电动舵机的数学模型。 |
| 6. | 8 . driver hardware of the ema is designed , with the schematic diagram of the corresponding components
设计了电动舵机驱动器硬件，给出了各组成部分的线路原理图。 |
| 7. | Fault diagnosis method based on recursive batch least square filter and its application to helicopter ' s electric rudders
递推批量最小二乘在直升机电动舵机故障诊断中的应用 |
| 8. | ( 2 ) relating the requirement of whole system , designed the experiment to check the execution mechanism of scgs - the characteristics of electrical step vane mechanism
结合全系统的要求，设计实验检查了航弹系统的执行机构? ?步进电动舵机的特性3 |
| 9. | This dissertation mainly investigates some robust control strategies of the electromechanical actuator which is supposed to be activated by the sinusoidal permanent magnet synchronous motor ( pmsm ) and limited angle torque motor ( latm )
本文主要研究了基于正弦波永磁同步电机( pmsm )及有限转角力矩电机( latm )驱动的电动舵机的鲁棒控制策略。 |
| 10. | The structure and principle of two different types of ema are systematically presented . the load characteristics and mechanical characteristics are analyzed with emphasis on the influence of the hinge torque on their dynamics and static characteristics
系统描述了两种不同类型的电动舵机的结构、工作原理，分析了其负载特性及机械特性，并着重讨论了铰链力矩对舵机动、静态特性的影响。 |
