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Descripción
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| The nature of numerical error is explained at the beginning of the chapter by separating it into local truncation and round-off error components. Advanced orbit propagation methods that based on regularizing and linearizing the equations of motion are described. One of these methods, based on regularized equations of motion for non-classical orbital elements, is applied to an analytical application for purposes of collision avoidance. | |
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Internacional
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Si |
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DOI
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10.2514/5.9781624103247.0049.0070 |
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Edición del Libro
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Editorial del Libro
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American Institute of Aeronautics and Astronautics, Reston, VA, USA |
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ISBN
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9781624103230 |
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Serie
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Progress in Astronautics and Aeronautics |
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Título del Libro
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Asteroid and Space Debris Manipulation: Advances from the Stardust Research Network |
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Desde página
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49 |
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Hasta página
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70 |