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基于SOPC的飞行器控制系统的硬件设计 被引量:8

Hardware Design of Flight Vehicle Control System Based on the SOPC
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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,较强的灵活性和较小的体积,提出了一种基于可编程片上系统(SOPC)技术的无人机飞行控制系统硬件解决方案;利用硬件描述语言在FPGA芯片内部编写了CAN总线控制器,配合Altera自带的IP核以及外围硬件电路,设计了一种基于SOPC的飞控系统;和传统的无人机控制系统相比其具有更高度集成性,并且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。 In order to cause the unmanned aerial vehicle flight control system has the formidable data-handling capacity,compared with the low power loss,compared with the strong flexibility and small volume,proposed one kind based on the programmable piece on the system(SOPC) technology unmanned aerial vehicle flight control system hardware-based solution.Has compiled the CAN bus control unit using the hardware description language in the FPGA chip,coordinates Altera bringing the IP nucleus as well as the periphery hardware circuit,has designed one kind based on the SOPC flight control system.Compares with the traditional unmanned aerial vehicle control system its has the high integration,and while having very strong data-handling capacity has the small volume and low power loss.The multiple flight proof,various modular design is reasonable,the overall system movement is stable,may serve as the next generation unmanned aerial vehicle high performance to apply the platform.
出处 《计算机测量与控制》 CSCD 北大核心 2010年第9期2112-2114,共3页 Computer Measurement &Control
关键词 无人机 NIOSⅡ SOPC FPGA UAV NIOSⅡ SOPC FPGA
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