Analytic Approximation for Fixed-Angle Constant Thrust Trajectories via Linear Perturbation Theory
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Veröffentlicht in: | Journal of guidance, control, and dynamics control, and dynamics, 2021-01, Vol.44 (1), p.163-171 |
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container_title | Journal of guidance, control, and dynamics |
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creator | He, Guanwei Melton, Robert G |
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doi_str_mv | 10.2514/1.G005303 |
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Published by the American Institute of Aeronautics and Astronautics, Inc., with permission. All requests for copying and permission to reprint should be submitted to CCC at www.copyright.com; employ the eISSN 1533-3884 to initiate your request. 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subjects | Aerospace engineering Approximation Coordinate transformations Earth Orbits Perturbation theory |
title | Analytic Approximation for Fixed-Angle Constant Thrust Trajectories via Linear Perturbation Theory |
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