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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
19860050600
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
August 12, 2013
Publication Date
January 1, 1985
Subject Category
Spacecraft Design, Testing And Performance
Accession Number
86A35338
Distribution Limits
Public
Copyright
Other

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