Mostrar el registro sencillo del ítem

dc.creatorYime-Rodríguez, E.
dc.creatorPeña-Cortés, C.A.
dc.creatorRojas-Contreras, W.M.
dc.date.accessioned2019-11-06T19:05:20Z
dc.date.available2019-11-06T19:05:20Z
dc.date.issued2014
dc.identifier.citationDYNA (Colombia); Vol. 81, Núm. 185; pp. 41-47
dc.identifier.issn0012-7353
dc.identifier.urihttps://hdl.handle.net/20.500.12585/8761
dc.description.abstractThe dynamic model of a Four Control Moment Gyroscope (4-CMG) is traditionally obtained after computing the derivative of the angular momentum equation. Although this approach leads to a simple dynamic model, new models have been introduced due to terms not taken into account during the computation of the angular momentum equation. In this paper, a new dynamic model for a 4-CMG based on the Newton-Euler algorithm, which is well accepted in Robotics, was developed. This new approach produces a complete dynamic model. © The authors; licensee Universidad Nacional de Colombia.eng
dc.format.mediumRecurso electrónico
dc.format.mimetypeapplication/pdf
dc.language.isoeng
dc.publisherUniversidad Nacional de Colombia
dc.rights.urihttp://creativecommons.org/licenses/by-nc-nd/4.0/
dc.sourcehttps://www2.scopus.com/inward/record.uri?eid=2-s2.0-84907353980&doi=10.15446%2fdyna.v81n185.35756&partnerID=40&md5=23f02227559fa594414975b17ca7f908
dc.sourceScopus 56368449100
dc.sourceScopus 56289654200
dc.sourceScopus 56367288700
dc.titleThe dynamic model of a four control moment gyroscope system
dc.title.alternativeModelo dinámico de un sistema de control de par por cuatro giróscopos
dcterms.bibliographicCitationKuhns, M., Rodriguez, A., Singularity avoidance control laws for a multiple CMG spacecraft attitude control system (1994) Proceedings of the American Control Conference (ACC), pp. 2892-2893
dcterms.bibliographicCitationKuhns, M., Rodriguez, A., A preferred trajectory tracking steering law for spacecraft with redundant CMGS (1995) Proceedings of the American Control Conference (ACC), pp. 3111-3115
dcterms.bibliographicCitationOh, S., Vadali, S.R., Feedback control and steering laws for spacecraft using single gimbal control moment gyros (1991) Astronautical Sciences, 39 (2), pp. 183-203
dcterms.bibliographicCitationThornton, B., Ura, T., Nose, Y., Turnock, S., Internal actuation of underwater robots using control moment gyros (2005) Proceedings of Oceans, pp. 591-598
dcterms.bibliographicCitationThornton, B., Ura, T., Nose, Y., Wind-up AUVs: Combined energy storage and attitude control using control moment gyros (2007) Proceedings of Oceans, pp. 1-9
dcterms.bibliographicCitationLappas, V.J., Steyn, W.H., Underwood, C.I., Torque amplification of control moment gyros (2002) IEEE Electronics Letters, 38 (15), pp. 837-839
dcterms.bibliographicCitationTekinalp, O., Elmas, T., Yavrucuk, I., Gimbal angle restricted control moment gyroscope clusters (2009) Proceedings of 4th International Conference On Recent Advances In Space Technologies (RAST), pp. 585-590
dcterms.bibliographicCitationFord, K.A., Hall, C.D., Singular direction avoidance steering for control-moment gyros (2000) Journal Guidance Control and Dynamics, 23 (4), pp. 648-656
dcterms.bibliographicCitationBedrossian, N.S., Paradiso, J., Bergmann, E.V., Rowell, D., Redundant single gimbal control moment gyroscope singularity analysis (1990) Journal Guidance Control and Dynamics, 13 (6), pp. 1096-1101
dcterms.bibliographicCitationToz, M., Kucuk, S., A comparative study for computational cost of fundamental robot manipulators (2011) Proceedings of International Conference On Industrial Technology (ICIT), pp. 289-293
dcterms.bibliographicCitationNegrean, I., Schonstein, C., Negrean, D.C., Negrean, A.S., Duca, A.V., Formulations in robotics based on variational principles (2010) Proceeding of International Conference On Automation Quality and Testing Robotics (AQTR), pp. 1-6
dcterms.bibliographicCitationTsai, L.W., (1999) Robot Analysis: The Mechanics of Serial and Parallel Manipulators, , Jon Wiley & Sons, Inc
dcterms.bibliographicCitationJaramillo, A., Franco, E., Guasch, L., Estimación de parámetros invariantes para un motor de inducción (2011) Dyna, 78 (169), pp. 88-94
dcterms.bibliographicCitationYime, E., Quintero, J., Saltaren, R., Aracil, R., A new Approach for Avoiding Internal Singularities in CMG with Pyramidal Shape Using Sliding Control (2009) Proceedings of European Control Conference (ECC), pp. 125-132
datacite.rightshttp://purl.org/coar/access_right/c_abf2
oaire.resourceTypehttp://purl.org/coar/resource_type/c_6501
oaire.versionhttp://purl.org/coar/version/c_970fb48d4fbd8a85
dc.type.driverinfo:eu-repo/semantics/article
dc.type.hasversioninfo:eu-repo/semantics/publishedVersion
dc.identifier.doi10.15446/dyna.v81n185.35756
dc.subject.keywordsControl
dc.subject.keywordsDynamics
dc.subject.keywordsGyroscope
dc.subject.keywordsModel
dc.rights.accessrightsinfo:eu-repo/semantics/openAccess
dc.rights.ccAtribución-NoComercial 4.0 Internacional
dc.identifier.instnameUniversidad Tecnológica de Bolívar
dc.identifier.reponameRepositorio UTB
dc.type.spaArtículo


Ficheros en el ítem

Thumbnail

Este ítem aparece en la(s) siguiente(s) colección(ones)

Mostrar el registro sencillo del ítem

http://creativecommons.org/licenses/by-nc-nd/4.0/
http://creativecommons.org/licenses/by-nc-nd/4.0/

Universidad Tecnológica de Bolívar - 2017 Institución de Educación Superior sujeta a inspección y vigilancia por el Ministerio de Educación Nacional. Resolución No 961 del 26 de octubre de 1970 a través de la cual la Gobernación de Bolívar otorga la Personería Jurídica a la Universidad Tecnológica de Bolívar.