摘要
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。
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.
出处
《电子技术应用》
北大核心
2013年第11期136-138,共3页
Application of Electronic Technique
关键词
多旋翼无人机
自主飞行
双芯片
系统设计
multi-rotor unmanned aerial vehicle
autonomous flight
dual chip
system design
