Method and apparatus for reaction wheel dynamic compensation...

Data processing: vehicles – navigation – and relative location – Vehicle control – guidance – operation – or indication – Aeronautical vehicle

Reexamination Certificate

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C244S158700, C244S165000, C244S164000, C244S169000

Reexamination Certificate

active

06990396

ABSTRACT:
A method and an apparatus for controlling the attitude and momentum of a spacecraft while deploying an appendage from the spacecraft. The method comprises the steps of predicting an environmental torque the spacecraft will be subjected to during deployment of the appendage, computing a magnitude and a direction of momentum to add to the spacecraft to at least partially oppose the predicted environmental torque, and storing the computed magnitude and direction of momentum in at least one of the momentum wheels before deploying the appendage.

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G.A. Kyroudis, “Survey of Solar-Sailing Configurations For Satellite Attitude Control,” AAS 91-486 pp. 815-838.

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