NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Identification of space shuttle main engine dynamicsSystem identification techniques are used to represent the dynamic behavior of the Space Shuttle Main Engine. The transfer function matrices of the linearized models of both the closed loop and the open loop system are obtained by using the recursive maximum likelihood method.
Document ID
19890010828
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Duyar, Ahmet
(Sverdrup Technology, Inc., Cleveland OH., United States)
Guo, Ten-Huei
(Sverdrup Technology, Inc., Cleveland OH., United States)
Merrill, Walter C.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 5, 2013
Publication Date
January 1, 1989
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
E-4680
NASA-TM-101982
NAS 1.15:101982
Meeting Information
Meeting: American Control Conference
Location: Pittsburgh, PA
Country: United States
Start Date: June 21, 1989
End Date: June 23, 1989
Sponsors: AIAA, AIChE, SCS, ASME, AISE, ISA
Accession Number
89N20199
Funding Number(s)
PROJECT: RTOP 582-01-11
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available