Results of a NASA sponsored study of V/STOL Propulsion Control Analysis are presented. The study involved propulsion control requirements, design concepts and procedures, and control designs for supersonic V/STOL. A variable cycle engine with a remote augmented lift system was used as a basis for establishing typical operating requirements and control concepts, and a nonlinear engine model was developed for control development as a precursor to a real-time simulation capability. A simplified aircraft model was also used to investigate transition requirements, and a long-range technology plan was developed to define subsequent program requirements for achieving a real-time piloted simulation capability.
V/STOL propulsion control technology
V/STOL Conference ; 1981 ; Palo Alto, CA
1981-12-01
Conference paper
No indication
English
V/STOL propulsion control technology
AIAA | 1984
|V/STOL propulsion control technology
AIAA | 1981
|V/STOL propulsion control technology
NTRS | 1984
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