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.
2019
ATTITUDE ESTIMATION; ANGULAR VELOCITY ESTIMATION; OPTICAL SENSORS
05 Brevetto::05a Brevetto
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).
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Utilizza questo identificativo per citare o creare un link a questo documento: https://hdl.handle.net/11573/1623760
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