queens-satellite-team / adcs

Simulation of satellite attitude based on reaction wheel model.
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adcs-66 - have gyros return current pos, accel, and vel. #105

Closed Aidan-Sheedy closed 1 year ago

Aidan-Sheedy commented 1 year ago

CHANGES

REASON Need position for the pointing mode controller. We can update the Gyro to be more accurate to the actual sensor later, for the controller all it cares about is the final result.

TESTING Compiles and can run unit tests.

GITHUB LINK https://github.com/queens-satellite-team/adcs/issues/66

Signed-off-by: Aidan-Sheedy Aidan.P.Sheedy@gmail.com