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Systematic Disturbance Of Optimal Rotational TrajectoryAlgorithm introduces systematic disturbance into otherwise optimal rotation of body from prescribed initial to prescribed final orientation. Disturbance introduced as deviation of actual axis of rotation from optimal one, like wobble of top. Algorithm effects rotational transformations and solves differential equations necessary to compute disturbed trajectory. Devised for use with motion-control program and three-dimensional computer-graphical display to study ability of observers to distinguish between optimal and suboptimal rotational trajectories.
Document ID
19920000539
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Grunwald, Arthur J.
(NASA Ames Research Center, Moffett Field, CA.)
Kaiser, Mary K.
(NASA Ames Research Center, Moffett Field, CA.)
Date Acquired
August 15, 2013
Publication Date
September 1, 1992
Publication Information
Publication: NASA Tech Briefs
Volume: 16
Issue: 9
ISSN: 0145-319X
Subject Category
Mechanics
Report/Patent Number
ARC-12700
Accession Number
92B10539
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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