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A Demonstration Advanced Avionics System for General Aviation
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English
Abstract
The Ames Research Center initiated a program in 1975 to provide the critical information required for the design of integrated avionics suitable for general aviation. The program has emphasized the use of data busing, distributed microprocessors, shared electronic displays and data entry devices, innovative low-cost sensors, and improved functional capability. Design considerations include cost, reliability, maintainability, and modularity. As a final step, a demonstration advanced avionics system is being designed, fabricated, and flight tested. The purpose of this paper is to provide a functional description of the Demonstration Advanced Avionics System including a description of the system architecture in order to document the direction that the program is taking.
Authors
- D. G. Denery - Ames Research Center, NASA Moffett Field, California
- G. P. Callas - Ames Research Center, NASA Moffett Field, California
- C. T. Jackson - Ames Research Center, NASA Moffett Field, California
- B. K. Berkstresser - Ames Research Center, NASA Moffett Field, California
- G. H. Hardy - Ames Research Center, NASA Moffett Field, California
Citation
Denery, D., Callas, G., Jackson, C., Berkstresser, B. et al., "A Demonstration Advanced Avionics System for General Aviation," SAE Technical Paper 790569, 1979, https://doi.org/10.4271/790569.Also In
References
- Denery D. G. Jackson C. T. Callas G. P. Berkstressor B. K. Hardy G. H. “Integrated Avionics for Future General Aviation Aircraft,” AIAA Paper 78-1482 AIAA Aircraft Systems and Technology Conference Los Angeles, Calif. Aug. 21-23 1978
- “NASA DAAS Phase I Functional Description,” Honeywell Inc. Feb. 1979