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NASA propulsion controls researchMultivariable control theory is applied to the design of multiple input and output engine controls. Highly-accurate, real-time engine simulations are utilized for control development and checkout. Electro-optical control components are developed for use in electronic control systems having fiber optic data links. Integrated controls are developed for VSTOL and Rotorcraft propulsion systems. Post-stall models of engine systems are developed to aid in understanding and control of post-stall engine behavior.
Document ID
19830017440
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Teren, F. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 4, 2013
Publication Date
January 1, 1983
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
E-1558
NAS 1.15:83343
NASA-TM-83343
Report Number: E-1558
Report Number: NAS 1.15:83343
Report Number: NASA-TM-83343
Meeting Information
Meeting: Intern. Symp. on Air Breathing Engines
Location: Paris
Start Date: June 6, 1983
End Date: June 11, 1983
Sponsors: International Society on Air Breathing Engines, Association Aeronautique et Astronautique de France
Accession Number
83N25711
Funding Number(s)
PROJECT: RTOP 505-40-5B
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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