Zobrazeno 1 - 10
of 12
pro vyhledávání: '"Carlos Renato Huaura Solórzano"'
Publikováno v:
The Scientific World Journal, Vol 2013 (2013)
The effects of a third-body travelling in a circular orbit around a main body on a massless satellite that is orbiting the same main body are studied under two averaged models, single and double, where expansions of the disturbing function are made,
Externí odkaz:
https://doaj.org/article/e64ffcd3f5784f34968cad5beca403ec
Publikováno v:
Biblioteca Digital de Teses e Dissertações do INPEInstituto Nacional de Pesquisas EspaciaisINPE.
Na literatura, existem diversos trabalhos que estudam os efeitos da perturbação de um terceiro corpo sobre um satélite. Alguns deles utilizam a hamiltoniana do sistema e outros utilizam a função perturbadora expressa em forma analítica. A prese
Externí odkaz:
http://urlib.net/cptec.inpe.br/walmeida/2003/08.21.09.35
Publikováno v:
Mathematical Problems in Engineering, Vol 2010 (2010)
For interplanetary missions, efficient electric propulsion systems can be used to increase the mass delivered to the destination. Outer planet exploration has experienced new interest with the launch of the Cassini and New Horizons Missions. At the p
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::06d8bd7a09956a22e501524e2490b98e
https://doi.org/10.1155/2010/313571
https://doi.org/10.1155/2010/313571
Publikováno v:
Advances in Space Research. 40:125-133
At the present time, the search for the knowledge of our Solar System continues effective. NASA’s Solar System Exploration theme listed a Neptune mission as one of its top priorities for the mid-term (2008–2013). From the technical point of view,
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::e267e04e4ca60bddaaf9b378ae922825
https://doi.org/10.1016/j.asr.2007.02.070
https://doi.org/10.1016/j.asr.2007.02.070
Publikováno v:
The Journal of the Astronautical Sciences. 54:583-593
Gravity assist is a proven technique in interplanetary exploration, as exemplified by the missions Voyager, Galileo, and Cassini. In the present paper, based in this well-known technique, an algorithm is developed to optimize missions to the outer pl
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::2e8a28d708d85d5f36c7b7f270bed560
https://doi.org/10.1007/bf03256507
https://doi.org/10.1007/bf03256507
Publikováno v:
Journal of Physics: Conference Series. 911:012012
The injection of a satellite into orbit is usually done by a multi-stage launch vehicle. Nowadays, the space market demonstrates a strong tendency towards the use of smaller satellites, because the miniaturization of the systems improve the cost/bene
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::4d64301ef64fb31a2b951cef642ec7d8
https://doi.org/10.1088/1742-6596/911/1/012012
https://doi.org/10.1088/1742-6596/911/1/012012
Publikováno v:
The Scientific World Journal, Vol 2013 (2013)
The Scientific World Journal
The Scientific World Journal
The effects of a third-body travelling in a circular orbit around a main body on a massless satellite that is orbiting the same main body are studied under two averaged models, single and double, where expansions of the disturbing function are made,
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::b577ecd23b41c0de46b4e225de60a8a2
Publikováno v:
Mathematical Problems in Engineering, Vol 2009 (2009)
Exploration of the outer planets has experienced new interest with the launch of the Cassini and the New Horizons Missions. At the present time, new technologies are under study for the better use of electric propulsion system in deep space missions.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::4f908f959505228b225af1c045d239f1
https://doaj.org/article/2a88f9d6a407442aa3fd1cb169c9d75f
https://doaj.org/article/2a88f9d6a407442aa3fd1cb169c9d75f
Publikováno v:
Mathematical Problems in Engineering, Vol 2007 (2007)
The Lagrange's planetary equations written in terms of the classical orbital elements have the disadvantage of singularities in eccentricity and inclination. These singularities are due to the mathematical model used and do not have physical reasons.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::22f720e8e684272f5757bd51152aef2c
https://doaj.org/article/324344f494094049aa5d16498f1af0e5
https://doaj.org/article/324344f494094049aa5d16498f1af0e5
Publikováno v:
56th International Astronautical Congress of the International Astronautical Federation, the International Academy of Astronautics, and the International Institute of Space Law.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::b91b4f6f400c1e5a01e891f836c5c7f8
https://doi.org/10.2514/6.iac-05-c1.p.23
https://doi.org/10.2514/6.iac-05-c1.p.23