Use este identificador para citar ou linkar para este item: http://repositorio.ufla.br/jspui/handle/1/46832
Registro completo de metadados
Campo DCValorIdioma
dc.creatorSilva, Felipe O.-
dc.creatorMenezes Filho, Rogério P.-
dc.creatorVieira, Leonardo A.-
dc.creatorKuga, Hélio K.-
dc.creatorBarros, Ettore A. de-
dc.date.accessioned2021-07-29T17:07:07Z-
dc.date.available2021-07-29T17:07:07Z-
dc.date.issued2020-10-
dc.identifier.citationSILVA, F. O. et al. Three-Axis Attitude Determination with Pseudo-Bias Estimation from Gravity/Magnetic Vector Observations. Journal of Guidance, Control, and Dynamics, Reston, v. 43, n. 12, Dec. 2020. DOI: https://doi.org/10.2514/1.G005253.pt_BR
dc.identifier.urihttps://doi.org/10.2514/1.G005253pt_BR
dc.identifier.urihttp://repositorio.ufla.br/jspui/handle/1/46832-
dc.description.abstractThis 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 method, purposely chosen to use nonunitary/nonorthogonal observations of the local gravity and Earth’s magnetic flux density vectors. For the simplifying assumption of body and navigation frames aligned, a comprehensive error analysis is developed, providing additional insight into the problem. Closed-form formulas for the residual normality and orthogonality errors are used to devise innovative pseudo-bias estimation (PBE) algorithms for the x- and z-axis magnetometer biases, as well as for the z-axis accelerometer bias. As a direct consequence of applying the latter, and also figuring as the main contribution of this paper, an improved (more accurate) AHRS stationary alignment approach is obtained, herein called TRIAD-PBE. The error analysis is extended to representative state-of-the-art attitude determination techniques, confirming the relevance of TRIAD-PBE, especially in the presence of hard-iron magnetism. Results from simulated and experimental tests confirm the adequacy of the outlined verifications.pt_BR
dc.languageen_USpt_BR
dc.publisherAmerican Institute of Aeronautics and Astronauticspt_BR
dc.rightsrestrictAccesspt_BR
dc.sourceJournal of Guidance, Control, and Dynamicspt_BR
dc.subjectMagnetometerspt_BR
dc.subjectAttitude and heading reference systempt_BR
dc.subjectAccelerometerpt_BR
dc.subjectMagnetic Fluxpt_BR
dc.subjectSingular value decompositionpt_BR
dc.subjectKalman filterpt_BR
dc.subjectEarth's magnetic fieldpt_BR
dc.subjectMonte Carlo experimentpt_BR
dc.subjectHistogramspt_BR
dc.subjectGravimetriapt_BR
dc.subjectMagnetômetrospt_BR
dc.subjectSistema de referência de atitude e orientaçãopt_BR
dc.subjectAcelerômetropt_BR
dc.subjectFluxo magnéticopt_BR
dc.subjectDecomposição em valores singularespt_BR
dc.subjectFiltro de Kalmanpt_BR
dc.subjectCampo geomagnéticopt_BR
dc.subjectMétodo de Monte Carlopt_BR
dc.titleThree-Axis Attitude Determination with Pseudo-Bias Estimation from Gravity/Magnetic Vector Observationspt_BR
dc.typeArtigopt_BR
Aparece nas coleções:DAT - Artigos publicados em periódicos
DEG - Artigos publicados em periódicos

Arquivos associados a este item:
Não existem arquivos associados a este item.


Os itens no repositório estão protegidos por copyright, com todos os direitos reservados, salvo quando é indicado o contrário.