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Optimal regulator or conventional? Setup techniques for a model following simulator control systemOptimal regulator technique was compared for determining simulator control system gains with the conventional servo analysis approach. Practical considerations, associated with airborne motion simulation using a model-following system, provided the basis for comparison. The simulation fidelity specifications selected were important in evaluating the relative advantages of the two methods. Frequency responses for a JetStar aircraft following a roll mode model were calculated digitally to illustrate the various cases. A technique for generating forward loop lead in the optimal regulator model-following problem was developed which increases the flexibility of that approach. It appeared to be the only way in which the optimal regulator method could meet the fidelity specifications.
Document ID
19780015077
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Deets, D. A.
(NASA Flight Research Center Edwards, CA, United States)
Date Acquired
August 9, 2013
Publication Date
January 1, 1978
Publication Information
Publication: NASA, Washington Fourth Inter-Center Control Systems Conf.
Subject Category
Research And Support Facilities (Air)
Accession Number
78N23020
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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