NASA NTRS · 19870008390
Optimal torque control for SCOLE slewing maneuvers
Abstract
The Spacecraft Control Laboratory Experiment (SCOLE) was slewed from one attitude to the required attitude and an integral performance index which involves the control torques was minimized. Kinematic and dynamical equations, optimal control, two-point boundary-value problems, and estimation of unknown boundary conditions are presented.
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Bainum, P. M., Li, Feiyue. 1987-01-01. Optimal torque control for SCOLE slewing maneuvers. https://ntrs.nasa.gov/citations/19870008390
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