An asymptotic solution for the main problem
| Data(s) |
2014
|
|---|---|
| Resumo |
In this paper, an analytical solution of the main problem, a satellite only perturbed by the J2 harmonic, is derived with the aid of perturbation theory and by using DROMO variables. The solution, which is valid for circular and elliptic orbits with generic eccentricity and inclination, describes the instantaneous time variation of all orbital elements, that is, the actual values of the osculating elements |
| Formato |
application/pdf |
| Identificador | |
| Idioma(s) |
eng |
| Publicador |
E.T.S.I. Aeronáuticos (UPM) |
| Relação |
http://oa.upm.es/37161/1/ADINVE_MEM_2014_197022.pdf |
| Direitos |
http://creativecommons.org/licenses/by-nc-nd/3.0/es/ info:eu-repo/semantics/restrictedAccess |
| Fonte |
AIAA/AAS Astrodynamics Specialist Conference : proceedings | 2014 AIAA/AAS Astrodynamics Specialist Conference | 4-7 Ago | San Diego, CA, USA |
| Palavras-Chave | #Aeronáutica #Física |
| Tipo |
info:eu-repo/semantics/conferenceObject Ponencia en Congreso o Jornada PeerReviewed |
