NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Rotorcraft flight-propulsion control integrationThe NASA Ames and Lewis Research Centers, in conjunction with the Army Research and Technology Laboratories have initiated and completed, in part, a joint research program focused on improving the performance, maneuverability, and operating characteristics of rotorcraft by integrating the flight and propulsion controls. The background of the program, its supporting programs, its goals and objectives, and an approach to accomplish them are discussed. Results of the modern control governor design of the T700 and the Rotorcraft Integrated Flight-Propulsion Control Study, which were key elements of the program, are also presented.
Document ID
19880007260
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Mihaloew, James R.
(NASA Lewis Research Center Cleveland, OH., United States)
Ballin, Mark G.
(NASA Ames Research Center Moffett Field, CA., United States)
Ruttledge, D. G. C.
(Sikorsky Aircraft Stratford, Conn., United States)
Date Acquired
September 5, 2013
Publication Date
February 1, 1988
Publication Information
Publication: NASA, Washington, NASA(Army Rotorcraft Technology. Volume 2: Materials and Structures, Propulsion and Drive Systems, Flight Dynamics and Control, and Acoustics
Subject Category
Aircraft Stability And Control
Accession Number
88N16643
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available