NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Rotorcraft flight-propulsion control integrationThe 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.
Document ID
19840063737
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Mihaloew, J. R.
(NASA Lewis Research Center Cleveland, OH, United States)
Chen, R. T. N.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
August 12, 2013
Publication Date
October 1, 1984
Publication Information
Publication: Vertiflite
Volume: 30
ISSN: 0042-4455
Subject Category
Aircraft Stability And Control
Report/Patent Number
ISSN: 0042-4455
Accession Number
84A46524
Distribution Limits
Public
Copyright
Other

Available Downloads

There are no available downloads for this record.
No Preview Available