一种无人机飞控计算机硬件平台的设计实现
作者:
作者单位:

1.中国飞行试验研究院 西安 710089;2.西安远方航空技术发展有限公司 西安 710089

中图分类号:

TP3


The Design and Implementation of a Small UAV Flight Control Computer Hardware Platform
Author:
Affiliation:

1.Chinese Flight Test Establishment, Xi'an 710089, China; 2. Xi'an Yuanfang General Aviation Technology Development Company Limited, Xi'an 710089, China

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    摘要:

    在对无人机飞控计算机技术发展应用叙述的基础上,设计了一款基于Zynq平台的应用于小型无人机的飞控计算机硬件平台。该硬件平台采用SOC处理架构,通过在单芯片上集成的双ARM硬核与外围FPGA实现了硬件外设的硬实时处理,极大的减轻了软件负担。文中对硬件平台的电源设计,气压高度、空速设计,接口设计等硬件单元进行了详细的描述。各项试验结果表明,此种架构的无人机飞控硬件平台集成度更高,尺寸更小,拓展能力极强,各设计单元均能实现预期目标且适用于恶劣的工作环境,对固定翼飞机具有很好的通用性。

    Abstract:

    Based on the development and application of UAV flight control computer technology, this paper designs a flight control computer hardware platform for small UAVs based on Zynq platform. The hardware platform adopts SOC processing architecture, realizes hard real-time processing of hardware peripherals through dual ARM hard cores and peripheral FPGA integrated on a single chip, which greatly reduces the software burden. This paper describes in detail The power supply design, air pressure altitude, airspeed design, interface design of the hardware platform. Various test results show that the UAV flight control hardware platform of this architecture has higher integration, smaller size, and strong expansion capability. Each design unit can achieve the expected goals and is suitable for harsh working environments. It has good versatility for fixed-wing aircraft.

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引用本文

罗霄,薛亚洲,张乐.一种无人机飞控计算机硬件平台的设计实现[J].电子测量技术,2021,44(1):50-54

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  • 在线发布日期: 2024-12-31
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