基本飞行控制系统的英文

• primary flight control system (pfcs)

• "基本"英文翻译    basic; fundamental
• "飞行"英文翻译    flight; flying; aviate; voya ...
• "控制系统"英文翻译    navar; control system; opera ...
• "基本飞行控制" 英文翻译 :    primary flight control (pfc)
• "飞行控制系统" 英文翻译 :    aircraft flight control systems; flight control system
• "初级飞行控制系统" 英文翻译 :    primary flight control system
• "辅助飞行控制系统" 英文翻译 :    secondary flight control system
• "冷气飞行控制系统" 英文翻译 :    cold gas flight control system
• "数字飞行控制系统" 英文翻译 :    digital flight control system
• "主要飞行控制系统" 英文翻译 :    pfcs primary flight control system
• "自动飞行控制系统" 英文翻译 :    automatic flight conrtol system; automatic flight control system
• "自组飞行控制系统" 英文翻译 :    self-organizing flight control system
• "综合飞行控制系统" 英文翻译 :    integrated flying control system
• "低温液体飞行控制系统" 英文翻译 :    cryogenic flight control system
• "飞行控制系统电子设备" 英文翻译 :    flight-control electronics; flight-control group electronic system
• "飞行控制系统根轨迹" 英文翻译 :    flight control system root locus
• "史密斯飞行控制系统" 英文翻译 :    smiths flight control system
• "应急飞行控制系统电门" 英文翻译 :    emergency flight control switch
• "运载火箭飞行控制系统" 英文翻译 :    monitor launch vehicle flight control system
• "增温率式飞行控制系统" 英文翻译 :    temperature rate flight control system
• "自动飞行控制系统接通" 英文翻译 :    afcs engagement
• "自适应飞行控制系统" 英文翻译 :    self adaptive flight control system
• "综合的飞行控制系统组件" 英文翻译 :    integral flight-control package
• "并行控制系统" 英文翻译 :    concurrent control system
• "共行控制系统" 英文翻译 :    concurrent control system

• Abstract : the control reconfigurable aircraft with multi - surfaces needs robust basic flight control system to support enough time for failure detection and isolation . when partial surface loses , it can keep the damaged aircraft stable . in this paper , multivariable output feedback digital control laws are designed for the control reconfigurable aircraft ( cra ) . the method uses fast - sampling digital pi controllers to design digital flight control tracking system . this paper gives the way to design the controller and analyze its robustness characteristics . the simulation results indicate that the controller is very robust and the output responses are fully satisfactory
  文摘:控制可重构飞机要求其基本飞行控制系统对舵面部分缺损故障具有强的鲁棒特性，在故障发生后保证飞机的稳定性，提供足够的时间进行故障的检测和隔离，为控制系统重构提供条件.本文采用高速采样pi控制器设计输出反馈跟随系统，给出了控制器的设计方法，并分析了它对于控制舵面部分缺损故障的鲁棒特性.仿真结果表明，这种控制器具有好的鲁棒特性