flight control的例句大全

An Intelligent Fault-Tolerant Flight Control Computer System Based on Serial Bus

一种基于串行总线的智能容错飞控计算机系统

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A new method to fulfill a flight control testing system is present.

给出了一种实现某飞控测试系统的新方法。

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μ Synthesis Design of Flight Control System for Robot Plane

无人机飞行控制系统的μ综合设计

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The disturbing factors play important roles on flight control system design.

各种干扰因素的影响对飞行控制系统设计起着不可忽视的作用。

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Application of Software Failure Modes and Effect Analysis Approach in Flight Control Software

SFMEA方法在飞行控制软件中的应用

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Study on Optical Fiber Temperature Sensor Used in Flight Control System by Light

一种用于光传飞控系统的光纤温度传感器研究

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Design of Flight Control System Using Improved Singular Perturbation Method

用改进的奇异摄动法设计飞行控制系统

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The model management system of flight control

飞行控制模型管理系统

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Study on Flight Control Law Based on Synthesized Nonlinear Control method

基于综合非线性控制方法的飞行控制律研究

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On fuzzy modelling of flight control system and its application

飞控系统的模糊模型及其研究

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Finally, this paper proves that the encapsulation of real-time CORBA object service can greatly help to develop UAH distributed flight control system by the result of distributed simulation experiment of sensor system.

最后，本文以传感器系统分布式仿真实验的结果证明，实时CORBA对象服务的组件化设计能为UAH分布式飞行控制系统的开发工作提供极大的帮助。

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An Optimization Design of Flight Control System of RPV

无人机飞行控制系统优化设计

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Research on Factors Effecting Control Accuracy of One channel Electrohydraulic Servo System Applied to Flight Simulation Turntable

影响仿真转台单通道电液位置伺服系统控制精度的因素探讨

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The control loading system is a very important subsystem in flight simulator.

操纵负荷系统是飞行模拟器的关键分系统之一.

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Air traffic control authorities will also unclear how the loss of Flight 007?

航空管制当局又怎么会不明不白的丢失了007航班?

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Design and Simulation of Flight Control System Based on LQG/ LTR Method

基于LQG/LTR方法的飞行控制系统设计与仿真

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Algorism Analysis of the Flight Control System Real Time Simulation

飞控系统实时仿真算法分析

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The equipments are RAMS 3000 intergrade control and display system for all weather & low altitude flight.

设备有用于全天候和贴地飞行的 RAMS3000 综合控制与显示系统.

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This paper introduces the research and application of flight dynamics in design of control augmentation system.

介绍了飞行力学在某型飞机控制增稳系统设计中的研究和应用.

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The method of nonlinear feedback linearization is applied to design and simulate the control laws for the aclinic flying climbing leveling flight state of an aircraft.

采用非线性反馈线性化设计方法对某型飞机进行了平飞爬升改平飞行状态控制律的设计和仿真。

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