飞控系统的英文

• afcs automatic flight control system
• fbw

• "飞"英文翻译    fly; flit
• "控"英文翻译    accuse; charge
• "系统"英文翻译    system
• "电传飞控系统" 英文翻译 :    fly-by-wire flight control system
• "动力飞控系统" 英文翻译 :    powered flight-control system
• "混合飞控系统" 英文翻译 :    hybrid flight-control system
• "数位飞控系统" 英文翻译 :    digital flight control system (dfcs)
• "数位飞控系统发展工具" 英文翻译 :    digital flight control system development tool
• "岸控系统" 英文翻译 :    shore control system
• "被控系统" 英文翻译 :    controlled system
• "不可控系统" 英文翻译 :    uncontrollable system
• "测控系统" 英文翻译 :    sda-n
• "程控系统" 英文翻译 :    program control system
• "调控系统" 英文翻译 :    regulator control system
• "非自控系统" 英文翻译 :    non autonomous system; nonautonomous system
• "光控系统" 英文翻译 :    light control system
• "环控系统" 英文翻译 :    ecs environmental control system
• "火控系统" 英文翻译 :    afcs; fire control systems; improved fire-control system-ifcs
• "甲烷控系统" 英文翻译 :    methane monitoring system
• "监控系统" 英文翻译 :    monitor system; monitored control system; monitoring control system; monitoring system; monitoring the system; supervisory system; supervisorysystem
• "键控系统" 英文翻译 :    keyed system
• "可控系统" 英文翻译 :    controllable system
• "联控系统" 英文翻译 :    xdvr
• "人控系统" 英文翻译 :    man-manageable system
• "施控系统" 英文翻译 :    controlling system

• Fuzzy controller design and stability analysis for flight control systems
  飞控系统模糊控制器设计及稳定性分析
• Fly - by - wire flight control system
  电传飞控系统
• Application of fuzzy mathematics in airplane flight control system ' s fault diagnosis
  模糊数学在飞机飞控系统故障诊断的应用
• On integrated design of fault detection and diagnosis modules in flight control systems
  飞控系统多种故障检诊模块的综合设计方法研究
• Conventional technology of pcs design cannot meet the requirements for quality design
  传统的飞控系统设计技术很难满足品质设计的要求。
• Design of a robust adaptive reconfigurable flight control system using multiple controllers
  基于鲁棒跟踪控制的飞控系统自适应重构技术研究
• Design of flight control system for helicopters based on inversion control technique and fuzzy logic
  基于逆控制和模糊逻辑的直升机飞控系统设计
• A design strategy based on state feedback and feedforward compensator for helicopter flight control system
  基于状态反馈及前置补偿策略的直升机飞控系统设计
• The simplified model is validated by verifying the main characteristics and functions of the fcs
  通过对飞控系统各项功能与特点的检验，对飞控系统简化模型进行了验证。
• The results indicate that the simplified model can satisfy the requirements of the fighter integrated design simulation system
  验证结果表明，所建立的简化飞控系统模型能够满足战斗机综合设计仿真系统的需要。