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A json file should exist in oresat-configs that defines all parameters needed (see examples in the python package)
Position will rely on GPS information. A TLE in oresat-configs may be used as a backup if GPS fails.
Attitude determination will rely on star tracker and model validation occurs with magnetometers and gyroscopes.
By default, the control software should only actuate the magnetorquers until the reaction wheels become more reliable. This restricts all missions to ones that can be accomplished with B-dot control.
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Here are a few notes on how the adcs package may eventually be implemented (https://github.com/oresat/oresat-adcs-software). The package needs more development before being implemented.
The text was updated successfully, but these errors were encountered: