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Descripción
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| An approximate analytical solution of the multiple revolution Lambert?s targeting problem is presented. The solution is obtained starting from Battin?s optimum single-impulse transfer with a linear phasing correction and offers remarkable accuracy near minimum delta-V transfer conditions. Consequently, the method is useful for rapidly obtaining low delta-V solutions for interplanetary trajectory optimization. The solution is easy to program and non-iterative, which makes it ideal for GPU implementation. In addition, the method can be employed to provide a fast first guess solution for enhancing the convergence speed of an accurate numerical multi-revolution Lambert solver. | |
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Internacional
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Si |
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Nombre congreso
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26th AAS/AIAA Spaceflight Mechanics Meeting |
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Tipo de participación
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960 |
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Lugar del congreso
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Napa, California |
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Revisores
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Si |
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ISBN o ISSN
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1081-6003 |
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DOI
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Fecha inicio congreso
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14/02/2016 |
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Fecha fin congreso
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18/02/2016 |
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Desde la página
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1 |
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Hasta la página
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14 |
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Título de las actas
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Advances in the Astronautical Sciences |