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Linearization of digital derived rate algorithm for use in linear stability analysisThe digital derived rate (DDR) algorithm is used to calculate the rate of rotation of the Centaur upper-stage rocket. The DDR is highly nonlinear algorithm, and classical linear stability analysis of the spacecraft cannot be performed without linearization. The performance of this rate algorithm is characterized by a gain and phase curve that drop off at the same frequency. This characteristic is desirable for many applications. A linearization technique for the DDR algorithm is investigated. The linearization method is described. Examples of the results of the linearization technique are illustrated, and the effects of linearization are described. A linear digital filter may be used as a substitute for performing classical linear stability analyses, while the DDR itself may be used in time response analysis.
Document ID
19850015593
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Graham, R. E.
(NASA Lewis Research Center Cleveland, OH, United States)
Porada, T. W.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 5, 2013
Publication Date
June 21, 1985
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
NASA-TM-87000
NAS 1.15:87000
E-2522
Report Number: NASA-TM-87000
Report Number: NAS 1.15:87000
Report Number: E-2522
Meeting Information
Meeting: Am. Control Conf.,
Location: Boston, MA
Country: United States
Start Date: June 19, 1985
End Date: June 21, 1985
Accession Number
85N23904
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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