Observatorio de I+D+i UPM

Descripción
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	Si
Nombre congreso	20th AAS / AIAA Space Flight Mechanics Meeting
Tipo de participación	960
Lugar del congreso	San Diego, California, EE.UU:
Revisores	Si
ISBN o ISSN	1081-6003
DOI
Fecha inicio congreso	14/02/2010
Fecha fin congreso	17/02/2010
Desde la página	2459
Hasta la página	2474
Título de las actas	Spaceflight Mechanics 2010, Vol. 136, Part I Advances in the Astronautical Sciences

Esta actividad pertenece a memorias de investigación

• Autor: Giulio Bau (Universidad de Padova, Italia)
• Autor: Claudio Bombardelli (UPM)
• Autor: Enrico Lorenzini (Universidad de Padova, Italia)
• Autor: Jesus Pelaez Alvarez (UPM)

• Creador: Departamento: Física Aplicada a la Ingeniería Aeronáutica