is negative if the principal axis of inertia targeted is the axis of maximum inertia of the spacecraft and is positive if the principal axis inertia targeted is the axis of minimum inertia of the spacecraft.
PROCÉDÉ ET DISPOSITIF DE CONTRÔLE D'ATTITUDE D'UN ENGIN SPATIAL
METHOD AND DEVICE FOR CONTROLLING ATTITUDE OF A SPACECRAFT
VERFAHREN UND VORRICHTUNG ZUR STEUERUNG DER STELLUNG EINES RAUMFAHRZEUGS
2019-07-31
Patent
Electronic Resource
French
PROCÉDÉ ET DISPOSITIF DE CONTRÔLE D'ATTITUDE D'UN ENGIN SPATIAL
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