Procédé et appareil de calibration des gyromètres d'un satellite stabilisé 3-axes

The procedure involves receiving position and attitude information from solar sensors (1), terrestrial and stellar sensors (3A,B) and gyroscopic meters (5). After treatment (21) the data and other orbital information (22) is processed by a Kalman filter which produces command signals to nozzle actua...

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Bibliographic Details
Main Authors PIERRE-YVES RENAUD, MICHEL SGHEDONI, ISSAM-MAURICE ACHKAR, PIERRE GUILLERMIN
Format Patent
LanguageFrench
Published 03.02.1995
Edition5
Subjects
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