ENERGY EFFICIENT SATELLITE MANEUVERING

Energy efficient satellite maneuvering is described herein. One disclosed example method includes maneuvering a satellite that is in an orbit around a space body so that a principle sensitive axis of the satellite is oriented to an orbit frame plane to reduce gravity gradient torques acting upon the...

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Bibliographic Details
Main Authors LEE, KANGSIK, LUI, TIMOTHY S
Format Patent
LanguageEnglish
French
Published 15.02.2022
Subjects
AIRCRAFT
AVIATION
COSMONAUTICS
PERFORMING OPERATIONS
TRANSPORTING
VEHICLES OR EQUIPMENT THEREFOR
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Summary:Energy efficient satellite maneuvering is described herein. One disclosed example method includes maneuvering a satellite that is in an orbit around a space body so that a principle sensitive axis of the satellite is oriented to an orbit frame plane to reduce gravity gradient torques acting upon the satellite. The orbit frame plane is based on an orbit frame vector. Il est décrit des manuvres de satellite à haut rendement énergétique. Un exemple décrit comprend manuvrer un satellite orbitant un astre de sorte quun axe sensible principal du satellite soit orienté vers un plan de cadre dorbite en vue de réduire les couples de gradient de gravité qui agissent sur le satellite. Le plan du cadre dorbite est basé sur un vecteur du cadre dorbite.
Bibliography:Application Number: CA20162941062