Process and device for aligning the roll axis of a satellite wit

Aeronautics and astronautics – Spacecraft – Attitude control

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Details

244171, 244173, 136246, B64G 136, B64G 144

Patent

active

044260520

ABSTRACT:
Device for aligning the roll axis of a rotating artificial satellite having radial solar panels equipped with angularly movable control surfaces at their extremities. The device includes a motor associated with each control surface for controlling the angle of the control surface with respect to the solar panel, each motor being actuated by a current which is dependent on the displacement of the roll axis from a desired position and which varies cyclically during the rotation of the satellite. The motor also includes a detector for detecting the angular speed of movement of the control surface and introducing a damping effect.

REFERENCES:
patent: 3116035 (1963-12-01), Cutler
patent: 3304028 (1967-02-01), Dryden
patent: 4161780 (1979-07-01), Rudolph et al.
patent: 4262867 (1981-04-01), Piening
patent: 4288051 (1981-09-01), Goschel

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