数据采集与处理2009，Vol.24Issue(z1)：233-236,4.
微小卫星星载处理器CAN接口设计与实现
Design and Realization of CAN Interface of CPU on Micro-satellite
赵小辉 1杨照华 1全伟1
作者信息
- 1. 北京航空航天大学仪器科学与光电工程学院,北京,100191
- 折叠
摘要
Abstract
The CAN bus is a commonly used system bus in the micro-satellite of astronautics with low-cost and high reliability.The ARM chip with low power consumption and high-performance is widely applied to spacecrafts.It develops the CAN interface of AT91RM9200 for two popular high-performance ARM9 chips without CAN.This paper designs and implements the hardware and the software of a CAN interface on the ARM processor based on the synchronous serial peripheral interface(SPI)of ARM and the CAN controller with the standard SPI interface.Finally,the CAN interface is tested in three Baud rates.Results show that the expansion using SPI interface of the CAN interface has a low power consumption and reliable performance.关键词
微小卫星/CAN总线/ARM/SPIKey words
micro-satellite/CAN bus/ARM/SPI分类
航空航天引用本文复制引用
赵小辉,杨照华,全伟..微小卫星星载处理器CAN接口设计与实现[J].数据采集与处理,2009,24(z1):233-236,4.
