The Ariel payload design post-PDR

Autor: Coyle, Laura E., Matsuura, Shuji, Perrin, Marshall D., Eccleston, Paul, Caldwell, Andrew, Bishop, Georgia, Desjonqueres, Lucile, Drummond, Rachel, Davidson, Alex, Whalley, Martin, Caldwell, Martin, Pearson, Chris, Simpson, Caroline, Fok, Sandy, Bruzzi, Davide, Davies, Alex, Anderson, Mark, Umesh, Pranav, Pascale, Enzo, Morgante, Gianluca, Focardi, Mauro, Savini, Giorgio, Ollivier, Marc, Rataj, Miroslaw, Malaguti, Giuseppe, Tinetti, Giovanna, Tozzi, Andrea, Chioetto, Paolo, Pace, Emanuele, Zuppella, Paola, Preti, Giampaolo, Serre, Christophe, Gomez, Jose M., Alonso, Gustavo, Perez, Javier, Bowles, Neil, Nowicki, Keith, Martignac, Jérôme, Berthé, Michel, Danto, Pascale, Crook, Martin, Hills, Matthew, Padley, Charles, Makinen, Semu, Kovacs, Zsolt, Szoke, Janos, Szirovicza, Peter, Sobiecki, Mateusz, Skup, Konrad, Wawer, Piotr, Ottensamer, Roland, Holmes, Warren, Goullioud, Renaud, Czupalla, Markus, Jessen, Niels Christian, Pedersen, Soren, Ray, Tom, Coffey, Deirdre, Steiger, Lukas, Compostizo, Carlos, Machado, Ricardo, Bocchieri, Andrea, Mugnai, Lorenzo, Birkmann, Stephan, Fahmy, Salma, Puig, Ludovic, Jollet, Delphine, Svedevall, Anders, Tirolien, Thierry, Salvignol, Jean-Christophe, Halain, Jean-Philippe

Publikováno v: Proceedings of SPIE; August 2024, Vol. 13092 Issue: 1 p130921B-130921B-21, 12961201p

Development of attitude determination sensors for miniature satellites

Autor: Svedevall, Anders

Attitude determination is an important subsystem of any satellite application. Several different approaches are available to determine the orientation of a spacecraft. By using a sun sensor, a pointing vector in the direction of the sun can be obtain

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=dedup_wf_001::ee723596b14a8461e58e5599e2580e76
http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-52057