Preliminary mission design for the next-generation infrared astronomical mission, SPICA,which is to be launched into the Sun-Earth L2 Halo orbit, was studied. Our specific focusis on investigating the impact of translational force (unloading ΔV), caused by thethruster unloading for accumulated angular momentum on the spacecraft reaction wheels,with respect to the orbit maintenance. In addition, suppression methods for orbitaldisturbances caused by the unloading ΔV are proposed and validated.
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