兵工自动化2017，Vol.36Issue(6)：90-92,96,4.DOI:10.7690/bgzdh.2017.06.023
某型无人直升机飞行控制系统半实物仿真
Semi-physical Simulation of Certain Type Unmanned Helicopter Flight Control System
高鹏飞 1郑云龙2
作者信息
- 1. 南京航空航天大学自动化学院,南京 210016
- 2. 中国人民解放军61330部队,河南新乡 453000
- 折叠
摘要
Abstract
Aiming at the actual demand of the performance ground test ofunmanned helicopter flight control system, research and design simulation platform for flight control performance test. Taking certain type "Single rotor coaxial fan" unmanned helicopter as example, gives the real-time working process of semi-physical simulation platform, establish math model according to dynamic knowledge, discuss design scheme, verify the platform function by hovering status simulation. The result show that the platform can similarly simulate the operating environment, verify the logic function and quality of the flight control system.关键词
无人直升机/飞行控制系统/半实物仿真Key words
unmanned helicopter/flight control system/semi-physical simulation分类
信息技术与安全科学引用本文复制引用
高鹏飞,郑云龙..某型无人直升机飞行控制系统半实物仿真[J].兵工自动化,2017,36(6):90-92,96,4.
