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한국항공우주학회지 = Journal of the Korean Society for Aeronautical & Space Sciences, v.35 no.7, 2007년, pp.647 - 654
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A Discrete continuation Method/homotopy approaches are studied for energy/fuel optimal low thrust Earth escape trajectory by solving a two point boundary value problem(TPBVP). Recently, maneuvers using low thrust propulsion system have been identified as emerging technologies. The low thruster is co...
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