Triaxially stabilized satellite provided with electric propulsors for orbital maneuvering and attitude control

摘要

The novelty consists precisely in the use of said electric, preferably ionic, propulsors, applied for the first time to satellite systems with multiple functions:   control of orbital parameters outside the plane (inclination and node);control within the plane of the orbit;altitude movements or any other type of orbital maneuver on triaxially stabilized satellites with an orbit LEO or GEO;attitude control during the phases of electric propulsion;desaturation of the wheels of inertia;etc...;The invention can be placed in the field of space technology and can be primarily applied in the field of satellites.