摘要
针对十字翼布局无人机飞行控制系统,设计该无人机半实物仿真系统,阐述了该系统的组成、原理,并介绍了仿真软件。通过对十字翼布局无人机飞行控制系统半实物仿真结果的分析和研究,验证了PID控制律能有效地控制十字翼布局无人机悬停阶段的姿态角和高度。结果表明仿真系统为自动驾驶仪的测试评估提供了平台和依据。
Direct at the flight control system of cruciform UAV,the hardware in the loop simulation system is designed. The composition and working theory of the system are formulated,and the formulation software is introduced. Through analysis and research of hardware in the loop simulation results of cruciform UAV flight control system,the PID control law is proved to be effective in controlling the attitude angle and height of cruciform UAV in hovering flight. The result shows that the system can provide a platform and foundation for test evaluation of autopilot.
出处
《现代电子技术》
2014年第5期18-20,共3页
Modern Electronics Technique
基金
国家自然科学基金项目(61273001)
