Solution of the Problem of Optimal Spacecraft Launching into Orbit Using Reactive Acceleration and Solar Sail in Kustaanheimo–Stiefel Variables |
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| Authors: | Sapunkov Ya G Chelnokov Yu N |
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| Institution: | 1.Institute of Precision Mechanics and Control Problems, Russian Academy of Sciences, 410028, Saratov, Russia
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| Abstract: | Cosmic Research - Using the Pontryagin maximum principle and the Kustaanheimo–Stiefel variables, the spatial problem of optimal launching into a given orbit of a spacecraft (SC) controlled by... |
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