Digital Avionics using Control Area Network
碩士 === 國立成功大學 === 航空太空工程學系碩博士班 === 95 === At the present, the small aircrafts are not equipped with high performance, high cost avionics data bus system. Based on performance enhancement, CAN bus is one of the most qualified candidate for future implementation into small aircrafts. This thesis stu...
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| Format: | Others |
| Language: | en_US |
| Published: |
2007
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| Online Access: | http://ndltd.ncl.edu.tw/handle/87162065257084771096 |
| Summary: | 碩士 === 國立成功大學 === 航空太空工程學系碩博士班 === 95 === At the present, the small aircrafts are not equipped with high performance, high cost avionics data bus system. Based on performance enhancement, CAN bus is one of the most qualified candidate for future implementation into small aircrafts. This thesis studies CAN bus system in application to small aircrafts for two function aspects: to improve flight instruments and to record flight data for performance recovery. This thesis verifies the system function capability from simulation and experiments. Some realist flight performance data from database are used for feasibility tests, and then high performance hardware CAN IP boards are introduced with suitable window displays for real experiment tests. The functions of windows display on line information, and execute fault detection at the same time. The monitor terminal is set as the highest priority node to broadcast all message and make revision the data bus operation to achieve CAN performance to small aircraft applications.
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