基于双STM32多旋翼无人机控制系统设计

提出一种基于双STM32芯片的控制系统设计方法和具体实现方案。控制系统以2个STM32F107VCT6芯片作为主从控制器，通过高速SPI接口进行数据通信，以保证控制阶段的实时性。介绍了系统的硬件布局，并且给出嵌入式系统的软件设计流程。实验结果证明，整个系统性能优良，为后续复杂的控制运算提供可靠的运作平台。...

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Bibliographic Details
Published in电子技术应用 Vol. 39; no. 11; pp. 136 - 138
Main Author 袁安富 徐金琦 王伟 马浩
Format Journal Article
LanguageChinese
Published 南京信息工程大学信息与控制学院,江苏南京,210044 2013
Subjects
双芯片
多旋翼无人机
系统设计
自主飞行
多旋翼无人机
autonomous flight
multi-rotor unmanned aerial vehicle
system design
自主飞行
系统设计
双芯片
dual chip
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ISSN0258-7998

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Summary:提出一种基于双STM32芯片的控制系统设计方法和具体实现方案。控制系统以2个STM32F107VCT6芯片作为主从控制器，通过高速SPI接口进行数据通信，以保证控制阶段的实时性。介绍了系统的硬件布局，并且给出嵌入式系统的软件设计流程。实验结果证明，整个系统性能优良，为后续复杂的控制运算提供可靠的运作平台。
Bibliography:A design method that based on double STM32 chips is proposed. The control system uses two STM32F107VCT6 chips to ensure the real-time performance, the communication between the two chips is completed by the high-speed SP[ interface. Additionally, the introduction of the system hardware layout and the software design flowchart detail is discussed. Tile experimental results demonstrate that the high-performance of the system, and provide a reliable operation platform fbr subsequent complex con- trol arithmetic.
Yuan Anfu, Xu Jinqi, Wang Wei, Ma Hao （School of Information and Control,Nanjing University of Information Science ＆ Technology, Nanjing 210044,China）
11-2305/TN
multi-rotor unmanned aerial vehicle; autonomous flight; dual chip; system design
ISSN:0258-7998