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Identification of propulsion systemsThis paper presents a tutorial on the use of model identification techniques for the identification of propulsion system models. These models are important for control design, simulation, parameter estimation, and fault detection. Propulsion system identification is defined in the context of the classical description of identification as a four step process that is unique because of special considerations of data and error sources. Propulsion system models are described along with the dependence of system operation on the environment. Propulsion system simulation approaches are discussed as well as approaches to propulsion system identification with examples for both air breathing and rocket systems.
Document ID
19930010920
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Merrill, Walter
(NASA Lewis Research Center Cleveland, OH, United States)
Guo, Ten-Huei
(NASA Lewis Research Center Cleveland, OH, United States)
Duyar, Ahmet
(Florida Atlantic Univ. Boca Raton., United States)
Date Acquired
September 6, 2013
Publication Date
August 1, 1991
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
NASA-TM-106007
NAS 1.15:106007
E-7171
Report Number: NASA-TM-106007
Report Number: NAS 1.15:106007
Report Number: E-7171
Accession Number
93N20109
Funding Number(s)
PROJECT: RTOP 506-42-72
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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