A PIC32 BASED FLIGHT CONTROL SYSTEM DESIGN FOR AN UAV

摘要：

In order to improve the performance of flight control system, a new flight control system design, based on PIC32 and real-time operating system μC/OS-II, oris proposed for a novel lighter than air unmanned aerial vehicle (UAV). This paper introduces the hardware structure and the interface and then analyzes the functions of different modules and the software flow. This design strategy reduces the system size, improves system reliability and simplifies the design complexity.

关键词： UAV flight control system PIC32 μC/OS-II

作者: BI XIAO-TAO

作者单位: School of Aeronautical Science and Engineering Beihang University Beijing, China

会议类型: 国际会议

会议名称: 3rd International Conference on Mechanical and Electrical Technology(ICMET2011) (2011第三届机械与电气技术国际会议)

会议地点: 大连

会议语种:英文

页码: 331-335

在线出版日期: 2011-08-26（万方平台首次上网日期，不代表论文的发表时间）