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Future challenges in V/STOL flight propulsion control integrationA survey of propulsion control requirements forming part of an advanced V/STOL control requirements study has to date determined, among other findings: (1) that the dependence of V/STOL flying qualities on propulsive lift makes it necessary to identify propulsion control requirements early in a development program; (2) that V/STOL controls of the future should relieve the pilot of control functions and elevate him to the position of a flight operations manager, with substantial gains in capability and/or safety; and (3) that research is required to define the V/STOL control system reliability requirements and specific component reliability allocations. An interactive, integrated design process for the realization of these objectives is also described.
Document ID
19810049766
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Roth, S. P.
(Pratt and Whitney Aircraft Group West Palm Beach, FL, United States)
Miller, R. J.
(United Technologies Corp. Pratt and Whitney Aircraft Group, West Palm Beach, Fla., United States)
Mihaloew, J.
(NASA Lewis Research Center Cleveland, Ohio, United States)
Date Acquired
August 11, 2013
Publication Date
October 1, 1980
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
SAE PAPER 801140
Report Number: SAE PAPER 801140
Meeting Information
Meeting: Aerospace Congress and Exposition
Location: Los Angeles, CA
Start Date: October 13, 1980
End Date: October 16, 1980
Sponsors: Society of Automotive Engineers
Accession Number
81A34170
Distribution Limits
Public
Copyright
Other

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