Attitude control for satellites

Aeronautics and astronautics – Spacecraft – Attitude control

Patent

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Details

244173, B64G 124

Patent

active

045911169

ABSTRACT:
The attitude control is provided under utilization of the solar wind in that the effective surface area of solar panels facing the sun is controlled in accordance with certain rules of asymmetry and under utilization of pulling cable so that an imbalance in received solar pressure is utilized to change the attitude of the satellite.

REFERENCES:
patent: 3863870 (1975-02-01), Andrews et al.
patent: 4426052 (1984-01-01), Huber et al.

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