飞行模拟转台

本文讨论FT型电动三轴飞行模拟转台微机实时控制软件的功能和实现方法。

This paper presents the properties and design techniques of the real time control software of the model FT series electric driven three axis flight simulator .

飞行模拟转台高精度数字重复控制器的设计

Design of High Precision Digital Repetitive Controller for Flight Simulator Servosystem

一种新的高精度数控3轴飞行模拟转台

A New High Precision Digital Control Three-axis Table for Flight Simulation

一种新型高性能单轴偏心液压飞行模拟转台的研制

A New High-performance Single-axis Hydraulic Flight Simulation Table with Eccentric Load

三轴飞行模拟转台实时控制软件的开发

Development on Real Time Control Software for Three Axis Flight Simulator

某飞行模拟转台伺服系统的摩擦模型仿真研究

Simulation Research on Friction Model of a Flight Simulation Table Servo System

三轴飞行模拟转台控制系统设计

Design of the Control System of Three Axes Flight Simulator

液压飞行模拟转台的数字自适应控制

Digital adaptive control of hydraulic flight simulation motion platform

三轴飞行模拟转台误差研究

Research on Error for a Three-Axis Flight Simulation Turntable

一种飞行模拟转台专用信号发生器

A Signal Generator Used for Flight Simulation Tables

计算机控制小型三轴飞行模拟转台

A Small Computer Controlled Flight Simulator with Three-axes

三轴飞行模拟转台的动态特性分析

Dynamic analysis of three - axis simulating table

三轴飞行模拟转台框架的优化设计

Structure Optimal Design of Three-Axis Simulating Table

飞行模拟转台伺服系统的改进

Improvement of servo systems for flight simulator

三维飞行模拟转台底座的建模和应力分析

Stress Analysis and Modeling of Turntable 's Basing Bracket by ANSYS and Pro / E

本文介绍了一种为三轴飞行模拟转台设计的新型液压伺服马达。

In this article , a new hydraulic servomotor designed for three axes flight simulator is introduced .

针对飞行模拟转台位置伺服系统中存在的非线性摩擦环节，设计了一种补偿摩擦的模糊边界层滑模变结构控制器。

This paper designs a fuzzy boundary layer sliding mode variable structure controller which can compensate the friction in the flight simulator servo system .

飞行模拟转台（亦称动态角运动模拟器）是飞机和导弹飞行控制系统地面飞行仿真试验的关键设备之一。

Dynamic angular motion simulator is one of the most important devices used in ground simulation tests for flight control systems of aircraft and guided missiles .

按照三轴飞行模拟转台实际运行情况，加载丰富的边界条件，采用拓扑优化分析方法对外环框架进行了结构优化分析。

The abundant boundary conditions are loaded on the outside framework according the true condition of simulation table operating and the Topology Optimization Analysis is applied to design the framework .

采用的研究手段有两种：一，以MATLAB/Simulink为平台进行仿真研究；二，利用捷联惯性组合和三轴飞行模拟转台，进行半实物实时在线实验研究。

Two kinds of research methods are adopted : one is simulating research based on MATLAB / Simulink , the other is the hardware-in-the-loop real-time simulation using strapdown inertial measurement unit ( SIMU ) which is composed of three FOGs and three accelerometers and three-axis rate table .

三轴飞行模拟仿真转台的设计及控制问题研究

Design and Research on Control Strategy of Three-axis Motion Simulator