复合控制系统的英文

• compound control system
• compound oxide series gas sensor
• multiplex control system

• "复合"英文翻译    compound; complex; composite ...
• "控制系统"英文翻译    navar; control system; opera ...
• "会合控制系统" 英文翻译 :    rendezvous control system
• "混合控制系统" 英文翻译 :    hcs hybrid control system
• "联合控制系统" 英文翻译 :    combined control system
• "拼合控制系统" 英文翻译 :    hybrid control system
• "综合控制系统" 英文翻译 :    combination control system; complex control system; integrated control system
• "组合控制系统" 英文翻译 :    combination control system
• "联合控制系统公司" 英文翻译 :    integrated control systems inc
• "汽车综合控制系统" 英文翻译 :    cacs comprehensive automobile control system; cacs compressive automobile control system; comprehensive automobile control system
• "潜艇综合控制系统" 英文翻译 :    submarine integrated control system
• "全综合控制系统" 英文翻译 :    fully integrated control system
• "数字调合控制系统" 英文翻译 :    digital blending control system
• "网络综合控制系统" 英文翻译 :    nics network integrated control system
• "战场综合控制系统" 英文翻译 :    integrated battlefield control system
• "复合控制" 英文翻译 :    combination control; compound control; multiplexed control
• "复合控制器" 英文翻译 :    combination controller
• "复合控制台" 英文翻译 :    composite console
• "复合控制酌" 英文翻译 :    compound control action
• "电能质量综合控制系统" 英文翻译 :    upqc
• "水面舰艇综合控制系统" 英文翻译 :    surface ship integrated control system
• "复合自动控制系统" 英文翻译 :    complex automatic control system
• "复合控制电压" 英文翻译 :    composite controlling voltage
• "复合控制作用" 英文翻译 :    compound control action; compoundcontrolaction
• "电话操作网络综合控制系统" 英文翻译 :    tonics telephone operations network integration control system; tonics telephone operations network integration control system

• Compound control system
  复合控制系统
• The simulation results show that the available load and the performance of the transit response improved obviously
  仿真结果显示，复合控制系统的可用过载和动态性能都有明显提高。
• The simulation results show that the available load and performance of transit response have improved obviously . 4
  仿真结果显示，复合控制系统的可用过载和动态性能都有明显提高。
• Two fuzzy neural network control systems are designed : fuzzy neural network self - learning control system and fuzzy neural cell complex control system
  分别设计了模糊神经网络自学习控制和模糊单神经元复合控制系统，并进行了计算机仿真。
• By means of guidance command decomposed forwardly , the combined control system is divided into two parallel subsystems : the aerodynamics subsystem and the direct force subsystem
  复合控制采用对制导指令进行前向分解的方法，将复合控制系统分为两个并行的子系统，即气动力控制子系统和直接力控制子系统。
• Next , the characteristics of the user satellites complex control system is that the high accuracy antenna pointing control is realized on the basis of ensuring the high accuracy attitude stabilization control of the satellite body
  3 .用户星复合控制系统的特点是在保证卫星平台高精度姿态稳定控制的前提下,实现星间链路天线的高精度指向控制。
• The results show that the performance of the combined control system designed in this thesis was superior to the traditional only aerodynamic control system , and the warhead of tactical ballistic missile with medium velocity could be intercepted
  结果表明，所设计的复合控制系统较纯气动力控制系统性能有所提高，能够拦截中等载入速的战术弹道导弹。
• 4 . the combined control system was designed . by means of control command decomposed forwardly , the combined control system was divided into tow parallel subsystems , namely the aerodynamics subsystem and the direct force subsystem
  复合控制系统采用对控制指令进行前向分解的方法，将复合控制系统分为两个并行的子系统，即气动力控制子系统和姿控直接力控制子系统。
• The antenna pointing control accuracy can satisfy the design specification and it is validated to be appropriate and effective . at last , the designed user satellites complex control system is simulated based on xpc target which is used for hardware - in - the - loop simulation
  4 .基于xpc实时仿真平台,充分利用实验室条件,搭建了用户星天线样机在回路中的半物理仿真实验,将天线指向控制系统和星体姿态稳定控制系统联合起来,组成中继卫星复合控制系统进行近一步的验证。
• To solve the problems caused by the varieties of the missile dynamics with the difference of flight height , velocity and attitude angle in modeling the missile , in this thesis , the theory of variable structure model reference adaptive control is used to design a pitch channel autopilot based on a longitudinal missile model , the status equation using the measurable parameters of load and angular rate is established , and the methodology to choosing the reference model is discussed also , and the performance of the controller is analyzed by means of simulation
  为了解决拦截弹气动参数随飞行高度、速度、姿态的不同，变化范围大，控制系统难以准确建模的困难，基于纵向平面拦截弹模型，采用模型参考变结构控制理论设计了俯仰通道姿控复合控制系统，以可测量变量过载和角速度作为状态量建立了系统的状态方程，讨论了参考模型的选择方法，并对系统的性能作了仿真分析。

• 复合控制系统的日语：ふくごうせいぎょシステム