The work described in this paper has been supported under NASA contract NAS1-18099, Integrated Airframe/Propulsion Control System Architecture (IAPSA II). This contract addresses methodology, analysis, and detailed design of integrated control system architectures suitable for high-performance aircraft of the 1990's. 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. This paper addresses the methodology and supporting tools.
Methods for evaluating integrated airframe/propulsion control system architectures
Methoden fuer die Auswertung integrierter Architekturen von Flugzeugzelle/Antriebssteuerungssystemen
1987
7 Seiten, 6 Bilder, 6 Quellen
Conference paper
English
Integrated Airframe Propulsion Control
NTIS | 1982
|Integrated airframe propulsion control
NTRS | 1982
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