Descripción
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A new formulation of the spacecraft relative motion for a generic orbit is presented based on the orbit propagation method proposed by Pelaez in 2006. We formulate the relative dynamics starting from a general form of the Clohessy-Wilthshire equations, where the orbital elements appear through the rotation matrix between the mobile and the inertial reference frame. The equations are than rewritten in function of the Pelaez variables in the special perturbation method. When compared with traditional relative motion proposed in the past the method offers better performance in terms of accuracy and computation speed. | |
Internacional
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Si |
Nombre congreso
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20th AAS / AIAA Space Flight Mechanics Meeting |
Tipo de participación
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960 |
Lugar del congreso
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San Diego, California, EE.UU: |
Revisores
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Si |
ISBN o ISSN
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1081-6003 |
DOI
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Fecha inicio congreso
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14/02/2010 |
Fecha fin congreso
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17/02/2010 |
Desde la página
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2459 |
Hasta la página
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2474 |
Título de las actas
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Spaceflight Mechanics 2010, Vol. 136, Part I Advances in the Astronautical Sciences |