现代电子技术2012，Vol.35Issue(10)：129-131,3.
基于SmartFusion的无人机飞行控制系统设计
Design of SmartFusion-based flight control system for UAVs
王昱辉 1雷金奎 2田力2
作者信息
- 1. 西北工业大学,陕西西安710129
- 2. 西北工业大学365研究所,陕西西安 710065
- 折叠
摘要
Abstract
In order to make the unmanned aerial vehicle flight control system has the formidable data-processing capacity, low power consumption* strong flexibility and small volume, a solution of unmanned aerial vehicle flight control system based on SmartFusion is proposed. The real-time opereational system (RTOS) pC /OS- II is adopted in the system to meet the realtime and stability needs of the flight control system. Compared with the control system of traditional unmanned aerial vehicle, it has higher integration and lower power consumption while having stronger data-handling capacity. The several flights prove that each modular design is reasonable, the overall system works stably, and the control system may serve as a high performance application platform for the next generation unmanned aerial vehicle.关键词
无人机/飞行控制系统/SmartFusion芯片/μC/OS-ⅡKey words
UAV/ flight control system? SmartFusion chip/ juC /OS-U分类
信息技术与安全科学引用本文复制引用
王昱辉,雷金奎,田力..基于SmartFusion的无人机飞行控制系统设计[J].现代电子技术,2012,35(10):129-131,3.
