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dc.contributor.authorGe, ZMen_US
dc.contributor.authorChen, HHen_US
dc.date.accessioned2019-04-02T06:00:30Z-
dc.date.available2019-04-02T06:00:30Z-
dc.date.issued1997-02-20en_US
dc.identifier.issn0022-460Xen_US
dc.identifier.urihttp://dx.doi.org/10.1006/jsvi.1996.0695en_US
dc.identifier.urihttp://hdl.handle.net/11536/149442-
dc.description.abstractAn analysis is presented for a single-axis rate gyro mounted on a space vehicle undergoing sinusoidal motion and steady rotation about its spin and output axes. By varying the amplitude of sinusoidal motion, the periodic and chaotic responses of this parametrically excited non-linear system are investigated using the incremental harmonic balance (IHB) method and numerical integration. The multi-variable Floquet theory is applied to analyze the stability of periodic attractors and the behavior of bifurcations. Additionally, phase portraits, Poincare maps, average power spectra, bifurcation diagrams, parametric diagrams and Lyapunov exponents are presented to observe Hopf bifurcation, symmetry-breaking bifurcations, period-doubling bifurcations and chaotic motions. The cell mapping technique (MICM) is also used to study the basins of attraction of periodic attractors. (C) 1997 Academic Press Limiteden_US
dc.language.isoen_USen_US
dc.titleBifurcations and chaotic motions in a rate gyro with a sinusoidal velocity about the spin axisen_US
dc.typeArticleen_US
dc.identifier.doi10.1006/jsvi.1996.0695en_US
dc.identifier.journalJOURNAL OF SOUND AND VIBRATIONen_US
dc.citation.volume200en_US
dc.citation.spage121en_US
dc.citation.epage137en_US
dc.contributor.department機械工程學系zh_TW
dc.contributor.departmentDepartment of Mechanical Engineeringen_US
dc.identifier.wosnumberWOS:A1997WK29000001en_US
dc.citation.woscount7en_US
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