摘要
自主飞行控制系统的设计对无人机的飞行特性有着至关重要的影响。详细的介绍了我所自主开发的无人机自动驾驶仪的研究进展,通过大量的数学仿真、地面半实物仿真和空中带飞试验,深入的考核了该驾驶仪的整体设计性能,同时经过带飞试验进一步验证所采用的PID控制方法的可行性,这为后续工作的深入开展奠定了基础。
The design of autonomous flight control system for UAV（Unmanned Aerial Vehicle） can greatly influence the flight performance.The review of the research on UAV autopilot was particularized.After finishing many mathematical simulations,hardware-in-the-loop simulations and flying testing,the design performance of this autopilot was assessed.And the flying experiments hanged on the plane prove that the PID regulation rule is feasible and effective.That also has laid a foundation for the future work.
出处
《系统仿真学报》
CAS
CSCD
北大核心
2009年第6期1716-1718,共3页
Journal of System Simulation
关键词
无人机
自主飞行
自动驾驶仪
PID控制
Unmanned Aerial Vehicle
Autonomous Flight
Autopilot
PID control
