System and method for attitude control and station keeping

Aeronautics and astronautics – Spacecraft – Attitude control

Reexamination Certificate

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C244S171200, C060S203100

Reexamination Certificate

active

07118075

ABSTRACT:
A system and method for supplying thrust to a structure, such as a satellite or spacecraft, for the purposes of station keeping and attitude control of the structure in low-gravity (orbital) and zero-gravity environments. The system includes devices for emitting energy beams and targets impacted by the energy beams to cause ablation of the targets. The beam-emitting devices and targets are adapted to cooperate and cause the structure to selectively undergo translational and/or rotational motion in reaction to the motion of material ablated from the targets. The position, alignment, and/or attitude of the structure can thereby be controlled in a zero or low-gravity environment by selectively emitting the energy beams at the targets.

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patent: 6945500 (2005-09-01), Wingo

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