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笔者首先介绍了四轴飞行器的机械结构及飞行原理,然后分析了飞行器控制系统的软硬件设计,最后探讨了飞行器姿态数据的获取与解算以及实现飞行器稳定飞行的控制算法,希望能够为今后相关问题的研究提供一定的参考依据。
The author firstly introduces the mechanical structure and flight principle of the quadcopter, then analyzes the hardware and software design of the aircraft control system. Finally, it discusses the acquisition and solution of the attitude data of the aircraft and the control algorithm to realize the stable flight of the aircraft. The study of the problem provides some reference.