Aeronautics and astronautics – Spacecraft – Attitude control
Patent
1988-05-16
1990-03-20
Basinger, Sherman D.
Aeronautics and astronautics
Spacecraft
Attitude control
244165, 244168, 244169, 244171, 244172, B64G 124
Patent
active
049094602
ABSTRACT:
Device and method for aiming a space probe toward a celestial body. It comprises a solar sail (30, 31) having an asymmetry about an axis (Z) and which subjects the probe (S) to a tilting torque of solar pressure. A kinetic wheel (20) turns about a perpendicular axis (X). This results in a rotation of the probe about the axis perpendicular to the two preceding axes (Y). The rotational speed of the wheel (20) is varied by a control system (23, 24) in order to change the rotational speed of the probe.
Application of the invention is to space probes that lie in the plane of the ecliptic.
REFERENCES:
patent: 4732354 (1988-03-01), Lievre
patent: 4767084 (1988-08-01), Chan et al.
Moura Denis
Torres Louis
Basinger Sherman D.
Centre National d'Etudes Spatiales
Sartelle Anne
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