Observatorio de I+D+i UPM

Descripción
An analytical solution of the two body problem perturbed by a constant tangential acceleration is derived with the aid of perturbation theory. The solution, which is valid for circular and elliptic orbits with generic eccentricity, describes the instantaneous time variation of all orbital elements. A comparison with high-accuracy numerical results shows that the analytical method can be effectively applied to multiple-revolution low-thrust orbit transfer around planets and in interplanetary space with negligible error.
Internacional	Si
JCR del ISI	Si
Título de la revista	Celestial Mechanics & Dynamical Astronomy
ISSN	0923-2958
Factor de impacto JCR	1,698
Información de impacto
Volumen	110
DOI
Número de revista
Desde la página	239
Hasta la página	256
Mes	SIN MES
Ranking

Esta actividad pertenece a memorias de investigación

• Autor: Claudio Bombardelli (UPM)
• Autor: Giulio Baú
• Autor: Jesus Pelaez Alvarez (UPM)

• Creador: Departamento: Física Aplicada a la Ingeniería Aeronáutica