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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 an autonomous flight control system has a crucial impact on the flight characteristics of the UAV. This paper introduces the research progress of autopilot of UAV autonomously developed by myself. It deeply tests the overall design performance of the autopilot through a large number of mathematical simulation, ground-floor semi-physical simulation and air-borne fly test. At the same time, Flight test to further verify the feasibility of the PID control method used, which laid the foundation for the follow-up work carried out in-depth.