DocumentCode
3731210
Title
Design of FlexRay-based communication on triplex redundancy flight control computer
Author
Junhua Chen; Dong Cao; Xunhong Lv
Author_Institution
College of Automation Engineering, Nanjing University of Aeronautics & Astronautics, China
fYear
2015
Firstpage
1969
Lastpage
1974
Abstract
To further improve the safety and reliability of small unmanned aerial vehicle (UAV), triplex redundancy flight control computer and its strategy of redundancy management were designed. And considering the limitations of communication speed and data communication load of traditional CAN bus, FlexRay-based communication mechanism has been designed. Specifically, mosular hardware has integrated the driver circuits, expanding FLASH and expanding RAM with the core board and its motherboard designed respectively, which is for the system upgrade and can protect the CPU. Then two-level redundancy management ideas of software vote and hardware arbitration were proposed in redundancy management design. Finally FlexRay bus was chosen to form the cross communication data link (CCDL) and to achieve communication mechanism among three channels. The analysis shows that the hardware design is reasonable, and the FlexRay-based CCDL can complete the data sharing of serial quantity, discrete quantity, analogue quantity, PWM quantity and state quantity in the design of 84 time slots with proper length.
Keywords
"Redundancy","Pulse width modulation","Switches","Manuals"
Publisher
ieee
Conference_Titel
Chinese Automation Congress (CAC), 2015
Type
conf
DOI
10.1109/CAC.2015.7382827
Filename
7382827
Link To Document