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A reusable rocket engine intelligent controlAn intelligent control system for reusable space propulsion systems for future launch vehicles is described. The system description includes a framework for the design. The framework consists of an execution level with high-speed control and diagnostics, and a coordination level which marries expert system concepts with traditional control. A comparison is made between air breathing and rocket engine control concepts to assess the relative levels of development and to determine the applicability of air breathing control concepts ot future reusable rocket engine systems.
Document ID
19890027610
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Merrill, Walter C.
(NASA Lewis Research Center Cleveland, OH, United States)
Lorenzo, Carl F.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
August 14, 2013
Publication Date
July 1, 1988
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
AIAA PAPER 88-3114
Accession Number
89A14981
Distribution Limits
Public
Copyright
Other

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