The parallel development of digital engine and flight controls for U.S. Army helicopters has made possible the future derivation of a fully integrated digital flight/propulsion control system. A NASA/Army research program has been undertaken to exploit these possibilities, ultimately yielding a generation of helicopters with exceptional agility and maneuverability in military roles and low pilot workloads in all-weather civil aviation missions. The program's three phases respectively address system modeling and analysis, flight hardware and software development, and flight evaluations aboard a research vehicle.
Rotorcraft flight-propulsion control integration
Vertiflite ; 30
1984-10-01
Miscellaneous
No indication
English
Rotorcraft flight-propulsion control integration
NTRS | 1988
|Rotorcraft Flight-Propulsion Control Integration
NTIS | 1988
|A rotorcraft flight/propulsion control integration study
NTRS | 1986
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