Satellite provided with means for countering solar pressure

Aeronautics and astronautics – Spacecraft – Attitude control

Reexamination Certificate

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Reexamination Certificate

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07624949

ABSTRACT:
A satellite intended to travel in a constellation of satellites in an area of space in which the dominant disturbing forces and torques are for the most part caused by differential solar pressure between the satellites of the constellation comprises a satellite structure and a sunshield to prevent at least a portion of the satellite structure from being illuminated by solar rays. The reflectivity of the reflective surfaces of the sunshield is adjusted as a function of the angle of incidence of the solar rays.

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T. Williams et al, “Solar radiation pressure and formation—keeping in highly elliptical orbits,” AIAA Astrodynamics Specialist Conference, vol. 1, Oct. 5, 2002, XP008044299.
T. Williams et al, “Uses of solar radiation pressure for satellite formation flight”, International Journal of Robust and Nonlinear Control, No. 12, 2002, pp. 163-183, XP002320333.
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L. Vaillon et al, “Precision formation flying design for the Smart-2 and Smart-3 technology demonstration missions”, Third International Workshop on Satellite Constellations and Formation Flying, Online! Feb. 24, 2003, pp. 91-99, XP002320334.

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