The invention concerns a method (1) for estimating the angular velocity (and, preferably, also the attitude) of a space platform (for example, a satellite, a space vehicle, or a space station) using only the information provided by one or more optical sensors, such as one or more star trackers (71, 72, 73), one or more colour and/or black and white cameras or video cameras, one of more infrared sensors, etc.
ESTIMATION OF ATTITUDE AND ANGULAR VELOCITY OF A SATELLITE BASED ON THE USE OF ONLY OPTICAL SENSORS / Cidonio, Emanuele; Curti, Fabio; Luchena, Daniele; Moriani, Marco; Spiller, Dario. - (2019).
ESTIMATION OF ATTITUDE AND ANGULAR VELOCITY OF A SATELLITE BASED ON THE USE OF ONLY OPTICAL SENSORS
CIDONIO, EMANUELE;CURTI, FABIO;MORIANI, MARCO;SPILLER, DARIO
2019
Abstract
The invention concerns a method (1) for estimating the angular velocity (and, preferably, also the attitude) of a space platform (for example, a satellite, a space vehicle, or a space station) using only the information provided by one or more optical sensors, such as one or more star trackers (71, 72, 73), one or more colour and/or black and white cameras or video cameras, one of more infrared sensors, etc.File allegati a questo prodotto
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