Zobrazeno 1 - 10
of 83
pro vyhledávání: '"Helio Koiti Kuga"'
Publikováno v:
Journal of Aerospace Technology and Management, Vol 5, Iss 4 (2013)
http://dx.doi.org/10.5028/jatm.v5i4.252 The nonlinear unscented Kalman filter (UKF) is evaluated for the satellite orbit determination problem, using Global Positioning System (GPS) measurements. The assessment is based on the robustness of the filt
Externí odkaz:
https://doaj.org/article/9650eae48db94495b558fdb4c97b0ef1
Autor:
Helio Koiti Kuga, Felipe O. Silva, Ettore Apolônio de Barros, Rogerio P. Menezes Filho, Leonardo A. Vieira
Publikováno v:
Journal of Guidance, Control, and Dynamics. 43:2237-2257
This paper revisits the stationary alignment problem of attitude and heading reference systems (AHRSs). The investigation is initiated from the three-axis attitude determination (TRIAD)–based metho...
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::a9313b762813b09cfbb20fb0747b0bf3
https://doi.org/10.2514/1.g005253
https://doi.org/10.2514/1.g005253
Autor:
Helio Koiti Kuga, Giancarlo Santilli, W. R. Silva, Paula Cristiane Pinto Mesquita Pardal, Maria Cecília Zanardi, Roberta Veloso Garcia
Publikováno v:
Scopus
Repositório Institucional da UNESP
Universidade Estadual Paulista (UNESP)
instacron:UNESP
Repositório Institucional da UNESP
Universidade Estadual Paulista (UNESP)
instacron:UNESP
Made available in DSpace on 2022-04-28T19:43:35Z (GMT). No. of bitstreams: 0 Previous issue date: 2022-04-01 Conselho Nacional de Desenvolvimento Científico e Tecnológico (CNPq) The Rao-Blackwellized Particle Filter (RaoBPF) and the Unscented Kalma
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::c736802b70a33e797789be650abaec08
Autor:
Helio Koiti Kuga, Roberta Veloso Garcia, Paula Cristiane Pinto Mesquita Pardal, Maria Cecília Zanardi
Publikováno v:
Repositório Institucional da USP (Biblioteca Digital da Produção Intelectual)
Universidade de São Paulo (USP)
instacron:USP
Universidade de São Paulo (USP)
instacron:USP
This article compares the attitude estimated by nonlinear estimator Cubature Kalman Filter with results obtained by the Extended Kalman Filter and Unscented Kalman Filter. Currently these estimators are the subject of great interest in attitude estim
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::520086b7b5d7770bc8bf24890276a006
https://doi.org/10.1016/j.asr.2018.10.003
https://doi.org/10.1016/j.asr.2018.10.003
The paper aims at discussing techniques for managing one implementation issue that often arises in the application of particle filters: sample impoverishment. Dealing with such problem can significantly improve the performance of particle filters, an
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::7a5f6a8f6a88a56887fd68ecabf01e02
This work has been submitted to the IEEE for possible publication. Copyright may be transferred without notice, after which this version may no longer be accessible.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::0a697c5632e4730b88526ec8744cb5cf
https://doi.org/10.36227/techrxiv.14465427.v1
https://doi.org/10.36227/techrxiv.14465427.v1
Publikováno v:
Ciências Exatas e da Terra: Aprendizado, Integração e Necessidades do País 2
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::a06763b9b8d4c76df43e782b89aa03ec
https://doi.org/10.22533/at.ed.6152114047
https://doi.org/10.22533/at.ed.6152114047
Publikováno v:
Ciências Exatas e da Terra: Aprendizado, Integração e Necessidades do País 2
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::5a91a95d12c599f367a69a368ac1c868
https://doi.org/10.22533/at.ed.6152114041
https://doi.org/10.22533/at.ed.6152114041
Publikováno v:
IEEE Transactions on Instrumentation and Measurement. 67:831-838
This paper presents an innovative in-field coarse bias estimation (CBE) method for stationary intermediate-grade inertial measurement units (IMUs), which is based on the existence of normality and orthogonality errors in the attitude matrix supplied
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::9ca1d5b6d4dfcc69b50baeba2a24f14b
https://doi.org/10.1109/tim.2017.2789138
https://doi.org/10.1109/tim.2017.2789138
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
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::1c3bba1c8827fe85f375ff12815bc2bf
https://doi.org/10.1016/j.measurement.2017.11.040
https://doi.org/10.1016/j.measurement.2017.11.040