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Dynamics of multirate sampled data control systemsThe effect was investigated of the synthesis approach (single or multirate) on the machine requirements for a digital control system for the space shuttle boost vehicle. The study encompassed four major work areas: synthesis approach trades, machine requirements trades, design analysis requirements and multirate adaptive control techniques. The primary results are two multirate autopilot designs for the low Q and maximum Q flight conditions that exhibits equal or better performance than the analog and single rate system designs. Also, a preferred technique for analyzing and synthesizing multirate digital control systems is included.
Document ID
19750005843
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Naylor, J. R.
(Boeing Aerospace Co. Seattle, WA, United States)
Hynes, R. J.
(Boeing Aerospace Co. Seattle, WA, United States)
Molnar, D. O.
(Boeing Aerospace Co. Seattle, WA, United States)
Date Acquired
September 3, 2013
Publication Date
October 1, 1974
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
NASA-CR-141458
D180-18438-1
Report Number: NASA-CR-141458
Report Number: D180-18438-1
Accession Number
75N13915
Funding Number(s)
CONTRACT_GRANT: NAS9-13690
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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