Zobrazeno 1 - 10
of 34
pro vyhledávání: '"Luiz S. Martins-Filho"'
Publikováno v:
Journal of Aerospace Technology and Management, Vol 12, Iss 1, Pp e3020-e3020 (2020)
This work deals with the problem of the design of an autonomous redundant system for the attitude determination of nanosatellites. The system consists of a circuit board equipped with three microcontrollers, a magnetic field sensor in three axes, an
Externí odkaz:
https://doaj.org/article/049f7a206e0841f4a017941623f42dee
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:
Luiz S. Martins-Filho, Jader de Amorim
Publikováno v:
Journal of Aerospace Technology and Management, Vol 8, Iss 1 (2016)
This article deals with the problem of Earth’s magnetic field sensors calibration in the context of low-cost nanosatellites’ navigation systems. The attitude of space vehicles can be determined from the state estimation using information from thr
Externí odkaz:
https://doaj.org/article/e4a56228cb924bd5825d5955f30f3830
Publikováno v:
Revista Brasileira de Ensino de Física, Vol 27, Iss 2, Pp 211-218 (2005)
Este artigo introduz um procedimento para o projeto de circuitos eletrônicos analógicos simples que emulam o comportamento dinâmico de sistemas físicos e matemáticos. Tais circuitos podem ser utilizados como uma aproximação experimental para d
Externí odkaz:
https://doaj.org/article/61ec9e271f7f41c596fbb4470e581e5e
Publikováno v:
Procedings do XV Simpósio Brasileiro de Automação Inteligente.
Publikováno v:
Journal of Aerospace Technology and Management v.12 2020
Journal of Aerospace Technology and Management
Departamento de Ciência e Tecnologia Aeroespacial (DCTA)
instacron:DCTA
Journal of Aerospace Technology and Management, Volume: 12, Article number: e3020, Published: 29 JUL 2020
Journal of Aerospace Technology and Management, Vol 12, Iss 1, Pp e3020-e3020 (2020)
Journal of Aerospace Technology and Management
Departamento de Ciência e Tecnologia Aeroespacial (DCTA)
instacron:DCTA
Journal of Aerospace Technology and Management, Volume: 12, Article number: e3020, Published: 29 JUL 2020
Journal of Aerospace Technology and Management, Vol 12, Iss 1, Pp e3020-e3020 (2020)
This work deals with the problem of the design of an autonomous redundant system for the attitude determination of nanosatellites. The system consists of a circuit board equipped with three microcontrollers, a magnetic field sensor in three axes, and
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::3cdc58d4a58ac9bcd36ae81c5e28f5d8
http://old.scielo.br/scielo.php?script=sci_arttext&pid=S2175-91462020000100329
http://old.scielo.br/scielo.php?script=sci_arttext&pid=S2175-91462020000100329
Autor:
Helio Koiti Kuga, Samuel R.C. Vale, Ricardo O. Duarte, Valdemir Carrara, Camila B.A. Garcia, Luiz S. Martins-Filho
Publikováno v:
Measurement. 116:391-401
This article presents an assessment step of the development of a fault tolerant attitude determination system (SDATF) for nanosatellites. This system will be flight validated as payload of the NanosatC-BR2, a 2U-size cubesat that is being developed b
Publikováno v:
Anais do 7. Congresso Brasileiro de Redes Neurais.
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:
Jader de Amorim, Luiz S. Martins-Filho
Publikováno v:
Journal of Aerospace Technology and Management v.8 n.1 2016
Journal of Aerospace Technology and Management
Departamento de Ciência e Tecnologia Aeroespacial (DCTA)
instacron:DCTA
Journal of Aerospace Technology and Management, Volume: 8, Issue: 1, Pages: 103-112, Published: MAR 2016
Journal of Aerospace Technology and Management
Departamento de Ciência e Tecnologia Aeroespacial (DCTA)
instacron:DCTA
Journal of Aerospace Technology and Management, Volume: 8, Issue: 1, Pages: 103-112, Published: MAR 2016
This article deals with the problem of Earth’s magnetic field sensors calibration in the context of low-cost nanosatellites’ navigation systems. The attitude of space vehicles can be determined from the state estimation using information from thr
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::84f8b90e98f3ea2f2796d185e68e6792
http://old.scielo.br/scielo.php?script=sci_arttext&pid=S2175-91462016000100103
http://old.scielo.br/scielo.php?script=sci_arttext&pid=S2175-91462016000100103