Zobrazeno 1 - 8
of 8
pro vyhledávání: '"Fernando Madeira"'
Publikováno v:
Journal of Aerospace Technology and Management, Vol 8, Iss 2, Pp 193-202 (2016)
Design candidates obtained from optimization techniques may have meaningful information, which provides not only the best solution, but also a relationship between object functions and design variables. In particular, trade-off studies for optimum ai
Externí odkaz:
https://doaj.org/article/ce3820d43fd24b128a624bc73a5901ad
Autor:
Antonio Gil Vicente de Brum, Annibal Hetem Jr., Israel da Silveira Rêgo, Cayo Prado Fernandes Francisco, Andre Fenili, Fernando Madeira, Flavio Caldas da Cruz, Marcelo Assafin
Publikováno v:
Journal of Aerospace Technology and Management, Vol 3, Iss 3, Pp 331-338 (2011)
The Brazilian deep space mission ASTER, as temporarily named, plans to send a small spacecraft to encounter and investigate the triple asteroid 2001-SN263. The launch is scheduled (initially) to occur in 2015, arriving in 2018. The main motivation of
Externí odkaz:
https://doaj.org/article/b3ed45ea3b864416910c0e7a37d9f20f
Autor:
Antonio Gil Vicente de Brum, Annibal Hetem Jr., Israel da Silva Rego, Cayo Prado Fernandes Francisco, André Fenilli, Fernando Madeira, Flávio Caldas da Cruz, Marcelo Assafin
Publikováno v:
Journal of Aerospace Technology and Management, Vol 3, Iss 3 (2012)
The Brazilian deep space mission ASTER, as temporarily named, plans to send a small spacecraft to encounter and investigate the triple asteroid 2001-SN263. The launch is scheduled (initially) to occur in 2015, arriving in 2018. The main motivation of
Externí odkaz:
https://doaj.org/article/b1136b9526b44174bce854aaed026942
Autor:
Fernando Madeira
Publikováno v:
Biblioteca Digital de Teses e Dissertações do ITAInstituto Tecnológico de AeronáuticaITA.
No presente trabalho uma nova técnica de programação não-linear, um método da projeção estocástica do gradiente, é aplicada para guiagem e controle não-linear em três dimensões de veículos lançadores de satélites, utilizando um modelo
Publikováno v:
Proceeding Series of the Brazilian Society of Computational and Applied Mathematics.
Trade-offs is one of important elements for engineering design problems characterized by multiple conflicting objectives that needs to be simultaneously improved. In this study, the real-coded Adaptive Range Multi-Objective Genetic Algorithm (ARMOGA)
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::baa1c8099bf87fa351d41f351d5728de
https://doi.org/10.5540/03.2016.004.01.0030
https://doi.org/10.5540/03.2016.004.01.0030
Publikováno v:
Journal of Aerospace Technology and Management, Volume: 8, Issue: 2, Pages: 193-202, Published: JUN 2016
Journal of Aerospace Technology and Management v.8 n.2 2016
Journal of Aerospace Technology and Management
Departamento de Ciência e Tecnologia Aeroespacial (DCTA)
instacron:DCTA
Journal of Aerospace Technology and Management, Vol 8, Iss 2, Pp 193-202 (2016)
Journal of Aerospace Technology and Management v.8 n.2 2016
Journal of Aerospace Technology and Management
Departamento de Ciência e Tecnologia Aeroespacial (DCTA)
instacron:DCTA
Journal of Aerospace Technology and Management, Vol 8, Iss 2, Pp 193-202 (2016)
Design candidates obtained from optimization techniques may have meaningful information, which provides not only the best solution, but also a relationship between object functions and design variables. In particular, trade-off studies for optimum ai
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::9a98a89ea828ab7bdfb5d2e2d3cc4b53
http://www.scielo.br/scielo.php?script=sci_arttext&pid=S2175-91462016000200193&lng=en&tlng=en
http://www.scielo.br/scielo.php?script=sci_arttext&pid=S2175-91462016000200193&lng=en&tlng=en
Autor:
Atair Rios-Neto, Fernando Madeira
Publikováno v:
Automatica. 36:427-438
A recently developed nonlinear programming stochastic projection of the gradient-type technique is applied to get and test novel procedures for tri-dimensional guidance and control of a satellite solid-fuel launch vehicle. Near optimal open-loop and
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::42c5751f69db0fccf2279e09cd233851
https://doi.org/10.1016/s0005-1098(99)00163-6
https://doi.org/10.1016/s0005-1098(99)00163-6
Autor:
Marcelo Assafin, Flavio C. Cruz, A. Hetem, Israel da Silveira Rêgo, Antonio G. V. de Brum, André Fenili, Fernando Madeira, Cayo Prado Fernandes Francisco
Publikováno v:
Journal of Aerospace Technology and Management, Volume: 3, Issue: 3, Pages: 331-338, Published: DEC 2011
Journal of Aerospace Technology and Management, Vol 3, Iss 3, Pp 331-338 (2011)
Journal of Aerospace Technology and Management, Vol 3, Iss 3, Pp 331-338 (2011)
The Brazilian deep space mission ASTER, as temporarily named, plans to send a small spacecraft to encounter and investigate the triple asteroid 2001-SN263. The launch is scheduled (initially) to occur in 2015, arriving in 2018. The main motivation of
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::e56e003f2051776912528db9b78b8dd9
http://www.scielo.br/scielo.php?script=sci_arttext&pid=S2175-91462011000300331&lng=en&tlng=en
http://www.scielo.br/scielo.php?script=sci_arttext&pid=S2175-91462011000300331&lng=en&tlng=en