NASA NTRS · 19830013989
Docking of a rigid spacecraft with unrestrained orbiting flexible structure
Abstract
A methodology for producing simulations of the docking of a rigid spacecraft with any unrestrained flexible structure was studied. A detailed algorithm for the simulation of the docking of a rigid body with a nonuniform unrestrained beam was sought. The values acquired during docking by the variables characterizing the motions of the rigid body and the unrestrained beam were sought.
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Kane, T. R.. 1983-04-01. Docking of a rigid spacecraft with unrestrained orbiting flexible structure. https://ntrs.nasa.gov/citations/19830013989
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