A laboratory-based testbed that will be used to explore various issues and concepts in spacecraft dynamics and control is described. The testbed is based on a triaxial air bearing to allow experiments involving large-angle, three-axis motion. The sensing, actuation, and processor hardware being developed for the testbed is highlighted.
Development of air spindle and triaxial air bearing testbeds for spacecraft dynamics and control experiments
American Control Conference, 2001 ; 3967-3972
2001
6 Seiten, 16 Quellen
Conference paper
English
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