Linearization methods for optimizing the low thrust spacecraft trajectory: Theoretical aspects |
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Authors: | P V Kazmerchuk |
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Institution: | 1.Federal Enterprise “Lavochkin Association”,Khimki, Moscow oblast,Russia |
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Abstract: | The theoretical aspects of the modified linearization method, which makes it possible to solve a wide class of nonlinear problems on optimizing low-thrust spacecraft trajectories (V. V. Efanov et al., 2009; V. V. Khartov et al., 2010) are examined. The main modifications of the linearization method are connected with its refinement for optimizing the main dynamic systems and design parameters of the spacecraft. |
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