四旋翼无人机飞行控制系统设计研究

谢龙;韩文波

【期刊名称】《光电技术应用》

【年(卷),期】2015(000)001

【摘要】Based on module thought, the controller, sensor, power supply, actuator and remote modules of four-rotor unmanned aerial vehicle (UAV) hardware system are introduced respectively in detail, and the relative circuit design is given. According to the hardware system requirements, an overall flowchart of flight control system soft?ware scheme is designed. With LabVIEW graphical language, the display interface based on four-rotor UAV flight control system is designed to collect the attitude angle data of four-rotor UAV in real time. Turret experiment analy?sis shows that the designed control system can meet the initial desired requirements and lays the theory foundation for further research.%根据模块化思想分别对四旋翼无人机[1]硬件系统的控制器模块、传感器模块、电源模块、执行机构模块以及遥控器模块[2-3]进行了详细的阐述，并给出了相应的电路设计。根据硬件系统所需的要求设计了飞行控制系统软件方案总体流程图，最后根据图形化语言LabVIEW设计了一套基于四旋翼无人机飞行控制系统的显示界面用来实时采集四旋翼无人机飞行器姿态角的数据[4]，通过转台实验分析证明，文中所设计四旋翼无人机飞行控制系统满足最初预期效果，为进一步研究奠定了理论基础。

【总页数】6页(48-53)