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   flight controls 的翻译结果: 查询用时:0.193秒
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flight controls
相关语句
  飞行控制
     In the dynamics simulation system frame, the plane's flight controls have two modes: hand-control and network-control.
     在此动力学仿真系统框架中,飞机的飞行控制分为两种方式:人工控制和网络控制。
短句来源
     Development of the electromechanical actuation system for use in primary flight controls is one of the major technologies in the path to an all electric airplane.
     飞行控制中机电作动系统的发展是全电飞机的重要技术之一 ,而无刷直流电动机是其中的关键部件 .
短句来源
  “flight controls”译为未确定词的双语例句
     Deep study of the decoupling control theory based on state variable method and simulation of the longitudinal and lateral-directional flight controls using this theory were performed.
     深入地研究了基于状态空间法的解耦控制理论,并用此理论对飞机的纵向和横航向的某一飞行 状态进行了仿真,得出了既可解耦也可以改善系统响应性能的控制方法。
短句来源
     Strudy and Simulation of Flight Controls Based on Decoupling Control Theory
     基于解耦控制的飞机飞行的控制方法仿真研究
短句来源
  相似匹配句对
     Memories in Flight
     飞行中的记忆
短句来源
     The Flight of Youth
     青春飞逝
短句来源
     Group C was controls.
     ③空白对照组 (C组 )。
短句来源
     Internal Controls
     内部控制
短句来源
     Strudy and Simulation of Flight Controls Based on Decoupling Control Theory
     基于解耦控制的飞机飞行的控制方法仿真研究
短句来源
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  flight controls
The emergence of these rare earth magnets allows SmCo motor-actuators for primary flight controls.
      
The captain then directed the check airman to take control of the throttles to free the captain and first officer to manipulate the flight controls.
      
There are three top-level modules hosting mission management, flight controls, and strap-down navigational software.
      
This computer has digital wiring running to the primary flight controls in the cockpit.
      
Some applications, such as remote sensing can tolerate transient upsets, while others such as flight controls cannot.
      
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Development of the electromechanical actuation system for use in primary flight controls is one of the major technologies in the path to an all electric airplane. Brushless DC motor(BLDCM) is the key in this system. In BLDCM designs, the use of samarium cobalt magnet can significantly reduce motor mass and increase efficiency. Such motor output of a high torque has a low rotor inertia, and quick responsibility.The machine volume is mainly limited by heating and a rise in temperature which results from...

Development of the electromechanical actuation system for use in primary flight controls is one of the major technologies in the path to an all electric airplane. Brushless DC motor(BLDCM) is the key in this system. In BLDCM designs, the use of samarium cobalt magnet can significantly reduce motor mass and increase efficiency. Such motor output of a high torque has a low rotor inertia, and quick responsibility.The machine volume is mainly limited by heating and a rise in temperature which results from the losses in the stator, it is independent of magnetic energy of PM materials. On the other hand, the use of pulse width modulation(PWM) inverter for BLDCM leads to a high increase of core loss. This paper presents the major electromagnetic factors of BLDCM, taking into account PWM inverter source, specification, power/mass and peak torque/rotor inertia etc.

飞行控制中机电作动系统的发展是全电飞机的重要技术之一 ,而无刷直流电动机是其中的关键部件 .采用钐钴永磁材料可以明显地减轻电机的质量和提高效率 ,该电机能在低惯量下输出高转矩 ,具有良好的快速响应能力 .但电机体积主要受定子损耗引起的发热和温升的限制 ,与永磁材料的磁能积无关 .另外 ,脉宽调制逆变器电源将使电机的铁损耗大大增加 .根据逆变器电源的特点 ,结合电机的技术指标和对功率 /质量、峰值转矩 /转子惯量等要求 ,提出了该电机设计时应考虑的主要电磁因素 .

This article introduces a new optimal designing version to counter the disturbance existed in multi -actuator hydraulic system for airplane with starting from the present situation of their developments and applications at home and abroad Flight controls-general should enjoy priority It is suitable on hydraulic system for aircraft,and will have stable and reliable work and broad application future

本文从国内外发展和应用的现状出发 ,针对飞机多执行器液压系统存在干扰的问题 ,介绍了一种优化设计方案 ,使飞机操纵系统有优先使用权。该方案对于所有飞机液压系统都适用 ,具有广泛的应用前景

Feedback linearization is a effective approach to a nonlinear control system. A major feature of next generation fighter aircraft is supermaneuver ability, and its control system must be a nonlinear control system. First, a feedback linearization theory is presented briefly, then the application of feedback linearization to flight controls is described. Finally simulation about anadvanced fighter aircraft are presented. According to the result of simulation,a conclusion can be made that the application...

Feedback linearization is a effective approach to a nonlinear control system. A major feature of next generation fighter aircraft is supermaneuver ability, and its control system must be a nonlinear control system. First, a feedback linearization theory is presented briefly, then the application of feedback linearization to flight controls is described. Finally simulation about anadvanced fighter aircraft are presented. According to the result of simulation,a conclusion can be made that the application to flight control systems is feasible and effective.

反馈线性化方法是一种有效的解决非线性系统控制的方法[1] 。而未来新一代战机控制系统需要适应超机动作战的非线性控制 ,非线性控制系统是必然要采用的。文中先简要介绍了反馈线性化理论 ,然后介绍了反馈线性化方法在飞控系统中的具体应用 ,最后以某型号先进战斗机为仿真算例进行了仿真 ,仿真结果表明 ,基于反馈线性化方法设计的飞控系统是可行的、有效的

 
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