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Mathematical Problems in Engineering
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2012
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Article
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Tab 5
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Research Article
Low-Thrust Out-of-Plane Orbital Station-Keeping Maneuvers for Satellites
Table 5
Errors allowed for final keplerian elements for Maneuver 2.
Semimajor axis
0.50 Km
Eccentricity
0.005
Inclination
0.001 deg