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基于SmartFusion的无人机飞行控制系统设计

Design of SmartFusion-based flight control system for UAVs

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【作者】 王昱辉雷金奎田力

【Author】 WANG Yu-hui,LEI Jin-kui,TIAN Li(1.Northwestern Polytechnical University,Xi’an 710129,China; 2.No.365 Research Institute,Northwestern Polytechnical University,Xi’an 710065,China)

【机构】 西北工业大学西北工业大学365研究所

【摘要】 为了使无人机飞行控制系统具有强大的数据处理能力、较低的功耗、较强的灵活性和更高的集成度,提出了一种以SmartFusion为核心的无人机飞行控制系统解决方案。为满足飞控系统实时性和稳定性的要求,系统采用了μC/OS-Ⅱ实时操作系统。与传统的无人机飞行控制系统相比,在具有很强的数据处理能力的同时拥有较小的体积和较低的功耗。多次飞行证明,各个模块设计合理,整个系统运行稳定,可以用作下一代无人机高性能应用平台。

【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) μC/OS-Ⅱis adopted in the system to meet the real-time 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.

  • 【文献出处】 现代电子技术 ,Modern Electronics Technique , 编辑部邮箱 ,2012年10期
  • 【分类号】V249.1
  • 【被引频次】7
  • 【下载频次】120
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