Design, development and flight test of a demonstration advanced avionics systemThe 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.
Document ID
19840006999
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Denery, D. G. (NASA Ames Research Center Moffett Field, CA, United States)
Callas, G. P. (NASA Ames Research Center Moffett Field, CA, United States)
Hardy, G. H. (NASA Ames Research Center Moffett Field, CA, United States)
Nedell, W. (NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
August 12, 2013
Publication Date
October 1, 1983
Publication Information
Publication: AGARD Advanced Concepts for Avionics(Weapon System Design, Develop. and Integration