直升机飞行模拟器及其特点  

Helicopter Flight Simulator and Its Characteristics

作　　者：袁东[1] 杨生民[1] 孙传伟[2] 

机构地区：[1]中国飞行试验研究院,西安710089 [2]南京航空航天大学,南京210016

出　　处：《系统仿真学报》2009年第9期2571-2573,共3页Journal of System Simulation

摘　　要：根据直升机与固定翼飞机飞行方式、操纵方式和任务使命的不同,简单叙述了直升机地面飞行模拟器研制的一般要求和特殊要求,并讨论了直升机飞行仿真模型的部件建模方法,特别是诱导速度模型和机身模型的特殊建模方法。最后给出了典型直升机地面飞行模拟器的飞行模拟曲线、分析以及飞行员评价,验证了模拟效果的可信性。According to the different of flight manner, control and mission between fixed wing plane and hehcopter, the general and specific requirements of the ground-based helicopter flight simulator were described, and the component modeling method of helicopter math model was discussed, especially the induced velocity and fuselage. Finally, the reliability of simulating results was validated by some curves of representative, its analysis and evaluation of test pilots.

关 键 词：直升机飞行模拟器 操纵负荷系统 部件建模法 诱导速度 

分 类 号：TP391.9[自动化与计算机技术—计算机应用技术]