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动态飞行仿真系统高载荷训练研究
引用本文:由俊生.动态飞行仿真系统高载荷训练研究[J].系统仿真学报,2002,14(11):1533-1535.
作者姓名:由俊生
作者单位:空军航空医学研究所,北京,100036
基金项目:空军重点项目基金([1998]办字1647号)
摘    要:介绍了动态飞行仿真系统的总体设计,结合现代军机的高载荷(高G值),飞行特点,详细介绍了高载荷飞行仿真的当前状况,从飞行仿真技术原理方案和载人离心机原理方案出发,采用了实时飞行仿真技术,直接力矩控制技术和交流同步电机驱动主心机的伺服调速体制,实现了高载荷(高G值)模拟飞行训练。

关 键 词:动态飞行仿真系统  高载荷训练  军用飞机  飞行员
文章编号:1004-731X(2002)11-1533-03
修稿时间:2002年1月10日

Research on High Acceleration Training of Dynamic Flight Simulation System
YOU Jun-sheng.Research on High Acceleration Training of Dynamic Flight Simulation System[J].Journal of System Simulation,2002,14(11):1533-1535.
Authors:YOU Jun-sheng
Abstract:The integrated design of dynamic flight simulation system is described in this paper. Combining the characteristic of high acceleration flight of modern military aircraft, the current situation of high acceleration flight is introduced in detail. According to the principle scheme of flight simulation technology and human centrifuge, using real-time flight simulation technology, servo timing control system of direct moment control technology and alternating synchronous motor driving, the high acceleration simulation flight training is accomplished.
Keywords:modern military aircraft  high acceleration  simulation  dynamic flight simulation system
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