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document
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Oomen, M.M. (author)
This thesis covers the design of the Attitude Control System for the SPS-2 configuration, developed at Airbus Defense and Space the Netherlands. The start of the SPS-2 mission consists of three phases: rate damping, Sun Acquisition and Sun Pointing. The SPS-2 satellite has five available mounting places for different payloads. In the first part...
master thesis 2016
Source URL (retrieved on 2024-06-02 13:17): https://repository.tudelft.nl/islandora/search/department%3A%22Astrodynamics%255C%20and%255C%20Space%255C%20Missions%22?collection=education&display=tud_default&f%5B0%5D=mods_subject_topic_ss%3A%22Airbus%22