Method and system for steering a momentum control system

Aeronautics and astronautics – Spacecraft – Attitude control

Reexamination Certificate

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C074S005340

Reexamination Certificate

active

10836986

ABSTRACT:
A momentum-control system comprising a plurality of momentum actuators and a platform upon which the plurality of momentum actuators are mounted. The momentum control system further comprises a plurality of active struts mounted on the bottom side of the platform. The active struts are configured to produce a force to steer the plurality of momentum actuators and the platform to produce forces and moments for spacecraft attitude control and disturbance suppression.

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patent: 6305647 (2001-10-01), Defendini et al.
patent: 6340137 (2002-01-01), Davis et al.
patent: 6354163 (2002-03-01), Heiberg

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