NASA NTRS · 19920000539
Systematic Disturbance Of Optimal Rotational Trajectory
Abstract
Algorithm 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.
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Grunwald, Arthur J., Kaiser, Mary K.. 1992-09-01. Systematic Disturbance Of Optimal Rotational Trajectory. https://ntrs.nasa.gov/citations/19920000539
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