摘要
航空发动机电子控制器采用CAN总线实现发动机控制系统与飞机综合控制系统通信，从硬件和软件两个方面对CAN总线在电子控制器中的应用进行了详细设计。电子控制器与飞机综控机调试结果表明CAN总线软硬件设计满足要求，为后续发动机控制系统的研制奠定良好基础。
The aeroengine electronic controller uses Can bus to realize the communication between the aero- engine control system and the aircraft integrated control system. The application of the CAN bus in the electron- ic controller is designed in detail from both hardware and software. The debugging results of the electronic con- troller and the aircraft integrated control system show that the CAN bus software and hardware design meets the requirements, which lays a good foundation for the development of the subsequent engine control system.
作者
邓佳
宋云峰
邓文革
任慧麟
DENG Jia;SONG Yun-feng;DENG Wen-ge;REN Hui-lin(AECC Hunan Aviation Powerplant Research Institute,Zhuzhou 412002,China)
出处
《测控技术》
CSCD
2018年第B11期425-427,共3页
Measurement & Control Technology
