The motivation was to develop a control design and analysis methodology directly applicable to design concepts of flexible spacecraft of interest the the U.S. Navy and to provide a testbed for the evaluation of large space structure control techniques developed at the Naval Research Laboratory. The topics covered include the following: (1) a list of key concepts; (2) evaluation of the Spacecraft Control Laboratory Experiment (SCOLE) model with DISCOS; (3) baseline results, line of sight error vs. time; (4) general formulation of optimization; (5) geometric interpretation, projected eigenaxis; (6) closed loop control law; and (7) future directions.
Minimum time slew of the SCOLE configuration
01.01.1984
Aufsatz (Konferenz)
Keine Angabe
Englisch
Slew Maneuvers on the Scole Laboratory Facility
NTIS | 1987
|Slew maneuvers on the SCOLE Laboratory Facility
NTRS | 1987
|Slew maneuver control of the spacecraft control laboratory experiment (SCOLE)
Tema Archiv | 1986
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