小型四旋翼无人机飞行控制系统设计与实现  

Design and implementation of flight control system for small quad-rotor

作　　者：李杰[1] 齐晓慧[1] 韩帅涛[1] 刘星海[1] 

机构地区：[1]军械工程学院无人机工程系,河北石家庄050003

出　　处：《中国测试》2014年第2期90-93,共4页China Measurement & Test

摘　　要：为进一步深入研究和开发小型四旋翼无人机搭建飞行控制实验系统,从硬件设计、软件开发和系统调试与飞行试验3个方面对搭建的小型四旋翼无人机飞行控制系统进行较为详细地阐述。飞行试验表明:所设计的飞行控制系统初步实现了对机体姿态的有效控制,为进一步研究自主飞行奠定了基础。The flight control experiment system was built for small quad-rotor so as to further research and development. This paper elaborated the flight control system for small quad-rotor in detail from three aspeets including hardware design, software design, and system debugging and flight tests. The flight tests show that the designed flight control system basically meets the needs of attitude control and lays a foundation for autonomous flight.

关 键 词：小型四旋翼无人机 飞行控制系统 硬件设计 软件设计 系统调试 飞行试验 

分 类 号：V279[航空宇航科学与技术—飞行器设计] V249