基于单片机的四旋翼飞行器的设计与实现

Design and Implementation of Four-rotor Aircraft Based on MCCM

四旋翼飞行器可以垂直升降,应用于军事和民用领域,在飞行器的设计中,结合单片机进行设计,可以提升整体性能。基于此,本文探究基于单片机的四旋翼飞行器设计与实现,探索飞行器的硬件设计和软件设计方案,并且对系统的角速度算法以及姿态控制算法进行测试,最后对系统的基础功能以及高级融合功能展开测试。经过测试发现,基于单片机的四旋翼飞行器设计具有可行性以及可靠性。希望通过本文的分析,可以为四旋翼飞行器的改进设计提供可行性借鉴。

Four-rotor aircraft can be lifted vertically and applied in the military and civilian fields.In the design of the aircraft,combined with the single-chip machine design,it can improve the overall performance.Based on this,this paper explores the design and implementation of MC-based quadrotor aircraft,explores the hardware design and software design scheme,tests the angular speed algorithm and attitude control algorithm,and finally tests the basic function and advanced integration fusion function of the system.The tests found that the MCbased four-rotor design has feasibility and reliability.It is hoped that the analysis of this paper can provide feasible reference for the improved design of four-rotor aircraft.