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dc.contributor.author Beyers, ME
dc.date.accessioned 2008-04-14T11:19:20Z
dc.date.available 2008-04-14T11:19:20Z
dc.date.issued 1975
dc.identifier.citation Beyers, ME. 1975. Technique for smoothing free-flight oscillation data. Journal of Spacecraft and Rockets, vol 12(5), pp 318-319 en
dc.identifier.issn 0022-4650
dc.identifier.uri http://hdl.handle.net/10204/2230
dc.description Copyright: 1975 American Institute of Aeronautics and Astronautics en
dc.description.abstract A technique based on superposition of tricyclic solutions has been proposed for smoothing free-flight angular motion. When incorporated into a conventional tricyclic data reduction program, the method is convenient to use and does not require a separate smooting routine. Tricyclic motion components determined in the smoothing process can be related to effects of individual nonlinearities on the motion. en
dc.language.iso en en
dc.publisher American Institute of Aeronautics and Astronautics en
dc.subject Oscillation data en
dc.subject Free-flight motion en
dc.title Technique for smoothing free-flight oscillation data. en
dc.type Article en


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