DIAGNOSIS OF HELICOPTER MODULAR AVIONICS
Abstract
The aim of the article is to present the analysis and processing of one of the avionics components in an avionics kit of helicopter BELL. At this time an avionics system on aircraft is complex structure and level of intelligent control has become important for trouble-free operation. The complexity, interconnection and cooperation of these systems is a difficult diagnosis which is time-consuming. Time is very important in aviation, let alone rescues the ingredients, which must be in a perfect technical background ready for immediate start for rescue. It is important to know to what extent and depth it is needed to integrate core system and the individual partial calculations break down into smaller subsystems. The aim of nowadays technology is less weight and better evaluation of capacity. Article is present device for easy and quick check of an avionic subsystem on the helicopter Bell 429.
Keywords
avionics device; control unit; data bus; shading; serial communication bus
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