Methodology, analysis, and detailed design of integrated control system architectures suitable for high-performance aircraft of the 1990s are presented. A methodology, with supporting analytical tools, has been developed to provide system designers with the capability to specify candidate architectures and accurately predict their reliability and performance in the early stages of design development. The authors address the methodology and supporting tools.
Methods for Evaluating Integrated Airframe/Propulsion Control System Architectures
IEEE National Aerospace and Electronics Conference (NAECON 87) ; 1987 ; Dayton, OH, US
1987-05-18
Conference paper
No indication
English
Methods for evaluating integrated airframe/propulsion control system architectures
Tema Archive | 1987
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