Method for orbital correction of an artificial satellite and corresponding device

Method for orbital correction of an artificial satellite and corresponding device

Orbital correction method and device for an artificial satellite. In order to stabilise the attitude of the satellite during the correction manoeuvre a polar stellar sensor 20 is used. The thrust axis 28 of the thruster 26 forms a defined angle with the pointing direction 22 of the polar sensor. App...

Ausführliche Beschreibung

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Bibliographische Detailangaben
1. Verfasser: PAUL ANDRE JULES DUCHON ET JEAN-MICHEL ADRIEN MARCEL GUILBERT
Format: Patent
Sprache:eng ; fre
Schlagworte:
AIRCRAFT
AVIATION
COSMONAUTICS
PERFORMING OPERATIONS
TRANSPORTING
VEHICLES OR EQUIPMENT THEREFOR
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Beschreibung
Zusammenfassung:Orbital correction method and device for an artificial satellite. In order to stabilise the attitude of the satellite during the correction manoeuvre a polar stellar sensor 20 is used. The thrust axis 28 of the thruster 26 forms a defined angle with the pointing direction 22 of the polar sensor. Application to geostationary satellites. PROCEDE ET DISPOSITIF DE CORRECTION D'ORBITE POUR SATELLITE ARTIFICIEL.POUR STABILISER L'ATTITUDE DU SATELLITE PENDANT LA MANOEUVRE DE CORRECTION ON UTILISE UN SENSEUR STELLAIRE DE POLAIRE 20. L'AXE DE POUSSEE 28 DU PROPULSEUR 26 FAIT UN ANGLE DETERMINE AVEC LA DIRECTION DE POINTAGE 22 DU SENSEUR DE POLAIRE.APPLICATION AUX SATELLITES GEOSTATIONNAIRES.