Observatorio de I+D+i UPM

Descripción
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.
Internacional	Si
DOI	10.2514/5.9781624103247.0049.0070
Edición del Libro
Editorial del Libro	American Institute of Aeronautics and Astronautics, Reston, VA, USA
ISBN	9781624103230
Serie	Progress in Astronautics and Aeronautics
Título del Libro	Asteroid and Space Debris Manipulation: Advances from the Stardust Research Network
Desde página	49
Hasta página	70

Esta actividad pertenece a memorias de investigación

• Autor: Davide Amato . (UPM)
• Autor: Claudio Bombardelli (UPM)

• Creador: Grupo de Investigación: Dinámica Espacial (SDG-UPM)
• Departamento: Física Aplicada a Las Ingenierías Aeronáutica y Naval