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- The parametric study of the in-plane Spacecraft Control Laboratory Experiment (SCOLE) system, the Floquet Stability Analysis, and three dimensional formulations of the SCOLE system dynamics are examined. Control issues are discussed, such as: control of large structures with delayed input in continuous time; control with delayed input in discrete time; control law design for SCOLE using Linear Quadratic Gaussian (LQC)/TRR technique; and optimal torque control for SCOLE slewing maneuvers.
- Other Subject(s):
- NASA Technical Reports Server (NTRS) Collection.
- Document ID: 19870008389.
Accession ID: 87N17822.
NASA. Langley Research Center Proceedings of the 3rd Annual SCOLE Workshop; p 11-67.
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