南京航空航天大学学报2017，Vol.49Issue(2)：219-224,6.DOI:10.16356/j.1005-2615.2017.02.011
无人直升机非线性飞行仿真建模与验证
Simulation and Validation of Unmanned Helicopter Nonlinear Model
王超 1贾伟力 1冯德利 1黄兵旺 1宫元 1计宏伟1
作者信息
摘要
Abstract
A nonlinear flight dynamics model is established for unmanned helicopter real-time simulation.As an example,the flight control law for an unmanned helicopter is designed.Hardware-in-loop simulation of hover maneuver flight and low speed flight is conducted,and the simulation results are compared with the flight test data.The simulation results agree well with the flight test data,thus proving the accuracy of nonlinear flight dynamics model.The attitude is controlled well during flight,and the rationality of control parameters is proved.关键词
无人直升机/飞行动力学/半物理仿真/飞行试验Key words
unmanned helicopter/flight dynamics/hardware-in-loop simulation/flight test分类
航空航天引用本文复制引用
王超,贾伟力,冯德利,黄兵旺,宫元,计宏伟..无人直升机非线性飞行仿真建模与验证[J].南京航空航天大学学报,2017,49(2):219-224,6.
