RAPID SLEW AND SETTLE SYSTEMS FOR SMALL SATELLITES

A new approach for rapid slew and settle of small satellites is based on four single degree-of-freedom control moment gyroscopes with variable speed flywheels (or reaction wheels) in a pyramid configuration, combined with path and endpoint constraint time-optimal control. The path and endpoint const...

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Hauptverfasser: Lim Sungyung, Tuohy Seamus, Duchesne Laurent, Dionne Daniel, Breger Louis
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creator Lim Sungyung
Tuohy Seamus
Duchesne Laurent
Dionne Daniel
Breger Louis
description A new approach for rapid slew and settle of small satellites is based on four single degree-of-freedom control moment gyroscopes with variable speed flywheels (or reaction wheels) in a pyramid configuration, combined with path and endpoint constraint time-optimal control. The path and endpoint constrained time-optimal control can be augmented with momentum management without the use of additional actuators.
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subjects AIRCRAFT
AVIATION
CONTROLLING
COSMONAUTICS
PERFORMING OPERATIONS
PHYSICS
REGULATING
SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
TRANSPORTING
VEHICLES OR EQUIPMENT THEREFOR
title RAPID SLEW AND SETTLE SYSTEMS FOR SMALL SATELLITES
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