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.
Docking of a rigid spacecraft with unrestrained orbiting flexible structure
01.04.1983
Aufsatz (Konferenz)
Keine Angabe
Englisch
Tether docking of orbiting spacecraft Final report
NTRS | 1971
|Tether Docking of Orbiting Spacecraft Final Report
NTIS | 1971
|