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Mathematical Problems in Engineering
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Mathematical Problems in Engineering
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2014
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Article
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Fig 2
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Research Article
Effects of the Eccentricity of a Perturbing Third Body on the Orbital Correction Maneuvers of a Spacecraft
Figure 2
Low thrust to correct the eccentricity for the maneuver from 0.02 to 0.01 using two arcs of propulsion.
(a)
(b)