The design of integrated avionics suitable for general aviation was examined. The program emphasizes the use of data busing, distributed microprocessors, shared electronic displays and data entry devices, and improved functional capability. Design considerations includes cost, reliability, maintainability, and modularity. A demonstration advanced avionics system (DAAS) was designed, built, and flight tested in a Cessna 402, twin engine, general aviation aircraft. The DAAS, and the system architecture are described.
Design, development and flight test of a demonstration advanced avionics system
1983-10-01
Conference paper
No indication
English
Demonstration Advanced Avionics System (Daas)
NTIS | 1982
F-4 Advanced Avionics Flight Test
AIAA | 1981
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