Unconstrained Direct Optimization of Spacecraft Trajectories Using Many Embedded Lambert Problems |
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| Authors: | Ottesen David Russell Ryan P |
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| Institution: | 1.Department of Aerospace Engineering and Engineering Mechanics, The University of Texas at Austin, 2617 Wichita Street, Austin, TX, 78712, USA
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| Abstract: | Journal of Optimization Theory and Applications - Direct optimization of many-revolution spacecraft trajectories is performed using an unconstrained formulation with many short-arc, embedded... |
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