飞行控制系统

大型飞行器动态飞行控制系统的仿真研究

Study on the Simulation of Large Scale Space Vehicle Dynamic Flying Control System

现代飞行控制系统的稳定鲁棒性评估

Robust Stability Estimate of Modern Flying Control System

基于多Agent的无人机自主飞行控制系统研究

Research on Autonomous Flight Control System for UAV Based on Multi-Agent System

C语言开发数字飞行控制系统软件

The Development of the Digital Flight Control System Operational Software Using c Language

基于PID控制器的鲁棒自动飞行控制系统设计

Design of Robust Flight Control System Based on PID Controller

基于USB的波分复用光传飞行控制系统的开发

WDM Fly-by-Light flight control system design based on USB

基于LMI的飞行控制系统H2/H∞状态反馈综合

LMI-Based H_2 / H_ ∞ State Feedback Synthesis for Flight Control System

直升机飞行控制系统鲁棒PI解耦设计

Robust PI decoupling design of helicopter flight control system

故障检测与隔离（FDI）、控制律重构是自修复飞行控制系统设计的重要内容。

Fault detection , isolation control reconfiguration are main designing content in self-repairing flight control system .

以某型直升机横航向通道为对象，将H∞控制理论与计算方法引入直升机飞行控制系统设计中。

In this paper , the H ∞ control theory is applied to design the flight control system of the helicopter lateral directional channel .

基于嵌入式计算机和MEMS传感器技术，构建了一个小巧的低成本飞行控制系统；

A low-cost and low-weight flight control system is developed based on embedded computing technology and MEMS sensors .

自修复飞行控制系统（SRFCS：Self-RepairingFlightControlSystem）是在电传飞控系统基础上发展起来的一种与主动容错技术结合的先进飞控系统，也是未来战斗机飞控系统的重要发展方向。

Self-Repairing Flight Control System ( SRFCS ) is a kind of active-and passive failure tolerant control based on the Fly-by-wire flight control system , and it is also an important tendency of the future flight control system .

基于组合导航技术，将陀螺仪数据与GPS接收数据进行了组合，提高了飞行控制系统导航的精度和可靠性。

Base on combine navigation technology , it improves the precision and reliability of the flight control system by combining the data recepted from both gyro and GPS .

基于RTOS的小型无人机飞行控制系统

A micro UAV control system based on RTOS

本文在分析中间件TAO及其服务机制基础上，研究无人直升机分布式飞行控制系统实现，利用TAO构建分布式仿真系统，以验证无人直升机分布式飞行控制系统设计。

In this paper , we study UH distributed flight control system based on the analysis of TAO and its service mechanism .

用PID控制器、近似神经网络动态逆模块、在线神经网络补偿器构建了飞行控制系统。

A new flight control system of the MAV was composed to two PID controllers , an approximate dynamic inversion block , and an adaptive on-line neural-network compensator .

采用加权灵敏度函数环路成形的H∞准则，给出了矢量推力喷管飞行控制系统的一种鲁棒控制器设计方法。

A methodology based upon the H ∞ principle of weighting sensitivity function loop - shaping is given to design the robust controller of flight control system for vector thrust nozzle .

针对直升机复杂的动力学特性和日益严格的操纵品质要求，应用二自由度H∞回路成形法设计了直升机鲁棒飞行控制系统。

Considering the complexity of helicopter flight dynamics and the rigorous flying quality requirement , the robust controller design of a helicopter was discussed using two degree of freedom H ∞ loop shaping control approach .

再次.研究了MAP与GPS及自动飞行控制系统（AFCS）的交连，设计出了GPS与MAP连接器电路图。

Thirdly the linking plan of MAP with GPS and automatic flight control system ( AFCS ) is given , A circuit diagram of GPS and MAP linking interface is presented .

再次，进行了飞行控制系统的软件设计与调试，包括陀螺A/D数据采样，PWM信号控制、GPS信号处理、RS232串口通讯电路等。

Third , it takes the design and debug of the software system , including of collecting data from gyro , PWM signal control , GPS signal processing and serial communication circuit .

B-2飞行控制系统的设计技术

Design Technique for B-2 Flight Control System

嵌入式计算机PC-104在飞行控制系统中的应用

An Application of Embedded Computer PC-104 in Flight Control System

根据UAV飞行控制系统的功能任务要求，提出了一种以ARM为控制核心、以CPLD为辅助控制器件的飞行控制方案。

According to the task requirement of flight control system for Unmanned Air Vehicles ( UAV ), a flight control scheme was proposed taking ARM processor as the core and CPLD as an assistant controller .

以主动颤振抑制系统设计为代表的气动伺服弹性力学（ASE）是一门涉及柔性结构、飞行器运动引起的定常和非定常气动力以及飞行控制系统相互作用的多学科技术。

Aeroservoelasticity , including active flutter suppression technology , is a multidisciplinary optimization technology that studies the interaction of flexible structure , unsteady aerodynamics and flight control system .

主要的内容包括直升机飞行控制系统内外回路设计、直升机机动飞行的仿真、地形跟随的仿真以及OpenGL三维动画仿真等方面的内容。

In this paper involved several aspects about the inner and outer loops design for helicopter flight control system , maneuver flight simulation for helicopter , terrain following simulation and 3D animation flight simulation system designed with OpenGL .

XV-15倾转旋翼飞机飞行控制系统概述

Flight control system development for the XV-15 tiltrotor aircraft

从MAV飞行控制系统的基本组成出发，讨论了MAV飞行控制器设计的性能评估准则、鲁棒性评估准则、安全性评估准则和控制能量准则。

From Micro Air Vehicle ( MAV ) flight control system 's basic constitution , this paper discusses MAV flight controller 's performance criteria , robustness criteria , security criteria and control energy criteria .

研究了综合火力／飞行控制系统（IFFCS）模糊控制器因子的自调整问题。

The self turning problem of the factors of fuzzy controller for integrated fire / flight control system ( IFFCS ) is studied .

在直升机显模型跟踪电传飞行控制系统（MFCS）的基础上，开发了直升机贴地飞行波分复用光传系统实时半物理仿真验证平台。

Based on the explicit model-following Fly-By-Wire ( FBW ) control system of the helicopter ( MFCS ), a real-time semi-physical nap-of-the-earth platform is established and a simulated fly test is processed .

针对一类多输入多输出非线性不确定系统，提出了基于模糊干扰观测器（FDO）的轨迹线性化控制（TLC）方法并应用于空天飞行器（ASV）飞行控制系统设计。

This paper presented an enhanced trajectory linearization control ( TLC ) method based on fuzzy disturbance observer ( FDO ) for a class of multi-input multi-output nonlinear uncertain system , and its application to an aerospace vehicle ( ASV ) flight control system .