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Integrated health monitoring and controls for rocket enginesCurrent research in intelligent control systems at the Lewis Research Center is described in the context of a functional framework. The framework is applicable to a variety of reusable space propulsion systems for existing and future launch vehicles. It provides a 'road map' technology development to enable enhanced engine performance with increased reliability, durability, and maintainability. The framework hierarchy consists of a mission coordination level, a propulsion system coordination level, and an engine control level. Each level is described in the context of the Space Shuttle Main Engine. The concept of integrating diagnostics with control is discussed within the context of the functional framework. A distributed real time simulation testbed is used to realize and evaluate the functionalities in closed loop.
Document ID
19930030657
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Merrill, W. C.
(NASA Lewis Research Center Cleveland, OH, United States)
Musgrave, J. L.
(NASA Lewis Research Center Cleveland, OH, United States)
Guo, T. H.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
August 15, 2013
Publication Date
April 1, 1992
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
SAE PAPER 921031
Report Number: SAE PAPER 921031
Meeting Information
Meeting: SAE, Aerospace Atlantic Conference
Location: Dayton, OH
Country: United States
Start Date: April 7, 1992
End Date: April 10, 1992
Sponsors: SAE
Accession Number
93A14654
Funding Number(s)
PROJECT: RTOP 506-42-72
Distribution Limits
Public
Copyright
Other

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