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Partially Invariant System for Spacecraft Center of Mass Motion Stabilization

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Figure

Figure 1.  Spacecraft with linear movement of PS in the inertial coordinate system
Figure 2.  Block diagram of a partially invariant spacecraft centre of mass stabilization system with linear movement of OD
Table 3.  Results of mathematical modeling for the invariant and standard systems for stabilization of Mars Orbital Sensing spacecraft
Figure 12.  Spacecraft X-axis angular deviation transition processes in the normal plane in an invariant stabilization system (deterministic model)
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