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propulsion control systems
相关语句
  推进控制系统
     THE EIGENVALUE SENSITIVITY ANALYSIS AND DESIGN FOR INTEGRATED FLIGHT/PROPULSION CONTROL SYSTEMS
     综合飞行/推进控制系统的特征值灵敏度分析和设计
短句来源
     This article presents analysis and optimized design to electromagnetic locking of automatic switch of the degaussing and electric propulsion control systems of degaussing ship. Further analysis is present on the circuit design and PLC software programming.
     文章对消磁船消磁、电力推进控制系统的自动开关电磁闭锁,从电路设计和PLC软件编程等方面进行了分析和优化设计。
短句来源
     A new regulating method is proposed which includes the influence of angle of attack, and is used to design an inlet ramp regulating system. Simulations show that the method is satisfactory, and it is important for the research of integrated flight/propulsion control systems.
     研究了将飞机攻角影响引入进气道斜板调节系统的调节规律,仿真结果表明该调节规律使斜板调节系统具有良好的性能,对深入研究综合飞行/推进控制系统具有重要作用。
短句来源
  “propulsion control systems”译为未确定词的双语例句
     Propulsion Control Specifications in Integrated Flight/Propulsion Control Systems
     在飞行/推进整体控制系统中推进控制的技术细则
短句来源
     H_∞ Control Applied in Integrated Flight and Propulsion Control Systems
     H_∞控制在飞行/推进综合控制系统中的应用
短句来源
     This paper deals with the application of advanced multivariable control technologies to integrated flight and propulsion control systems.
     研究了多变量控制技术应用于飞行/推进一体化控制器的设计问题。
短句来源
  相似匹配句对
     F, as control.
     F,对照组。
短句来源
     Computerised Propulsion Control
     计算机控制推进
短句来源
     U. in control.
     U.
短句来源
     The Propulsion Control and Simulation Research of the Submarine
     潜艇的推进控制及仿真研究
短句来源
     Analysis of Autonomous Intelligent Control Techniques for Spacecraft and Its Propulsion Systems
     空间飞行器及其推进系统智能自治控制技术分析
短句来源
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  propulsion control systems
The authors propose a solution for the analysis of robust stability and performance in identifying variability in propulsion control systems.
      


In this paper, sensitivity approaches are taken to analyse and design an integrated flight/propulsion control system where the interaction between subsystems directly affects the stability property and handling performances of the aircraft. The eigenvalue sensitivity approach is employed to study the effect of coupling parameters on system stability and gain sensitivity approach is used to direct the reduced states feedback sub-optimal control system design. Simulation results shew that...

In this paper, sensitivity approaches are taken to analyse and design an integrated flight/propulsion control system where the interaction between subsystems directly affects the stability property and handling performances of the aircraft. The eigenvalue sensitivity approach is employed to study the effect of coupling parameters on system stability and gain sensitivity approach is used to direct the reduced states feedback sub-optimal control system design. Simulation results shew that the integrated flight/propulsion control system designed by sensitivity approaches is of good performance.

在综合飞行/推进控制系统中,子系统之间的相互作用对飞机的稳定性、控制和性能具有直接的影响。本文应用特征值灵敏度分析法研究耦合系数的大小对系统稳定性的影响;应用增益灵敏度分析,进行减状态反馈次优设计,仿真结果表明设计合理,方法可行。

A Tactical Flight Management (TFM)system has been developed that incorporates system concepts for enroute navigation, energy management, threat penetration, terrain following/terrain avoidance, and advanced maneuvering weapon delivery. Flight management technology to automatically couple advanced weapon delivery capability to the flight control system has been developed in the Integrated Flight/Weapon Control program. Approaches to coupling the navigation system to the flight...

A Tactical Flight Management (TFM)system has been developed that incorporates system concepts for enroute navigation, energy management, threat penetration, terrain following/terrain avoidance, and advanced maneuvering weapon delivery. Flight management technology to automatically couple advanced weapon delivery capability to the flight control system has been developed in the Integrated Flight/Weapon Control program. Approaches to coupling the navigation system to the flight control and propulsion control system have been studied in the Integrated Flight Trajectory Control program. Advanced penetration concepts have been investigated in the Advanced Terrain Following/Terrain Avoidance. A Tactical Flight Management system is described which builds and expands on these technology foundations to develop a unified, full-mission system which significantly improves effectiveness and survivability.

本文着重介绍战术飞行管理系统的概念、要求和展望。战术飞行管理系统是最近才提出的区域导航、能量管理、突防、地形跟踪/回避、提高机动武器效能的综合系统概念。把提高武器效能自动地与飞行控制系统交联的飞行管理技术已发展成综合飞行/武器控制,而导航系统、飞行控制系统及推力控制系统的交联则涉及综合飞行轨迹控制,现代突防概念要研究地形跟踪/回避。战术飞行管理系统是在这些技术基础上发展一个统一任务使命系统,以明显提高作战效能和生存性.

This paper describes the propulsion control system based on instantaneous spatial vector control theroy. By controlling the output of the non-zero vectors, the flux in the motor gap will run along a polygon, which approximates a circle; by controlling the output of zero vectors on the side of the polygon, the mean voltage and the mean frequency of the inverter are varied as expected. In order to avoid the vertical force affects as disturbance to levitation system, the constant slip control...

This paper describes the propulsion control system based on instantaneous spatial vector control theroy. By controlling the output of the non-zero vectors, the flux in the motor gap will run along a polygon, which approximates a circle; by controlling the output of zero vectors on the side of the polygon, the mean voltage and the mean frequency of the inverter are varied as expected. In order to avoid the vertical force affects as disturbance to levitation system, the constant slip control method is adopted. This system is fully digitized by the microprossor-MCS8098, and the results of running test for low power motor are presented.

论述了运用瞬时空间电压矢量理论研制的磁浮车直线电机牵引控制系统,通过控制非零空间电压矢量的输出,使电动机气隙磁通沿准圆形轨迹运行;通过对准圆形轨迹上的零电压矢量的控制,改变逆变器的平均电压和平均频率。为消除单边直线电机垂直力的影响,采用恒定转差频率控制。系统由8098单片机实现,并进行了电机小功率运行实验

 
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