Review on Key Techniques of Dynamics Modeling for Helicopter Simulator

作     者：Gu Hongbin Fu Jun Hu Jinshuo 

作者机构：Research Center of Flight Simulation and Advanced Engineering TrainingCollege of Civil AviationNanjing University of Aeronautics and Astronautics 

出 版 物：《Transactions of Nanjing University of Aeronautics and Astronautics》 (南京航空航天大学学报（英文版）)

年 卷 期：2016年第33卷第6期

页      面：-页

核心收录：

学科分类：08[工学] 082503[工学-航空宇航制造工程] 0802[工学-机械工程] 0825[工学-航空宇航科学与技术] 0704[理学-天文学] 

基　　金：supported by the Fundamental Research Funds for the Central Universities the Research Innovation Program for College Graduates of Jiangsu Province(No.KYLX_0294) 

主　　题：helicopter dynamic model off-aixs response 

摘      要：We review the state of the art of dynamic modeling methods for helicopter *** dynamic models,including ARMCOP,GENHEL,FLYRT,BEMAP,F-B412 and UTIAS,are *** address off-axis response problem by focusing on flexible blade model,Pitt-Peters dynamic inflow model,Peters-He finite state inflow model and free wake model which are integrated with the baseline *** the advances in computing power,efficient free-vortex algorithms and parallel processing,free wake model can be used to simulate in real-time and significantly improves the effectiveness of solving off-axis response problem.