Monitoring and data acquisition system for experimental general aviation fly‐by‐wire aircraft
A CAN data bus was used in a project of an experimental Fly‐by‐Wire control system (SPS‐1) mounted on board a PZL‐110 “Koliber” general aviation aircraft. This solution allows the free communication between flight control computers and individual modules of the system. The monitoring of the bus stat...
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| Format: | Article |
| Language: | English |
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Vilnius Gediminas Technical University
2008-09-01
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| Series: | Aviation |
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| Online Access: | https://journals.vgtu.lt/index.php/Aviation/article/view/7392 |