System and method for assessing the performance of an attitude control system for small satellites
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United States of America Patent
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Nov 24, 2015
Grant Date -
Aug 8, 2013
app pub date -
Jul 7, 2011
filing date -
Jul 14, 2010
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Abstract
Various embodiments of the present invention include systems and methods for assessing the performance of an actuator of a attitude control system (ACS), such as a control moment gyroscope (CMG). In one embodiment, a system includes a support bracket assembly coupled to an actuator, wherein the actuator is configured to generate an output torque. The system also includes at least one sensor assembly coupled to the support bracket assembly, wherein the at least one sensor assembly includes a sensor configured to measure the output torque about at least one axis of the support bracket assembly while the support bracket assembly remains substantially motionless.
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