SEDSAT - II ADCS

Purdue SEDS is designing and building an Attitude Determination and Control System (ADCS) for use on the new SEDS cubesat. The new SEDSAT will be a pico-sat, meaning it has a mass of 1 kg or less. Having such a small satellite is a cheap and efficient way to get into space, but it presents several challenges for miniaturizing the technologies needed for attitude control.

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