Search NASA⌕ Search

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.

Keep this discovery

Explore connections, maps & timelines

BibTeXRIS

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

Cite the original work for its findings. Save a collection to share your selection of sources.