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Cat-2 Assembly, Integration and Verification
(AIV) activities of the Engineering Model (EM)
and the Flight Model (FM) are being carried out at
present. The Attitude Determination and Control
System (ADCS) and Flight Software (FSW)
validation campaigns will be performed at
Universitat Politècnica de Catalunya (UPC)
during the incomings months. An analysis and
verification of the 3Cat-2 key mission
requirements has been performed. The main
results are summarized in this work.
CitationCarreño-Luengo, H., Amezaga, A., Bolet, A., Vidal, D., Jané, J., Muñoz, J., Olive, R., Camps, A., Carola, J., Catarino, N., Hagenfeldt, M., Palomo, P., Cornara, S. 3CAT-2: a 6U CibeSat-based multi-constellation, dual-polarization, and dual-frequency GNSS-RO experimental mission. A: IEEE International Geoscience and Remote Sensing Symposium. "2015 IEEE International Geoscience & Remote Sensing Symposium: proceedings: July 26–31, 2015: Milan, Italy". Milan: 2015, p. 5115-5118.
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