Please use this identifier to cite or link to this item: https://doi.org/10.4050/JAHS.57.012004
DC FieldValue
dc.titleComprehensive nonlinear modeling of a miniature unmanned helicopter
dc.contributor.authorCai, G.
dc.contributor.authorChen, B.M.
dc.contributor.authorLee, T.H.
dc.contributor.authorLum, K.-Y.
dc.date.accessioned2014-04-24T08:34:00Z
dc.date.available2014-04-24T08:34:00Z
dc.date.issued2012-01
dc.identifier.citationCai, G., Chen, B.M., Lee, T.H., Lum, K.-Y. (2012-01). Comprehensive nonlinear modeling of a miniature unmanned helicopter. Journal of the American Helicopter Society 57 (1) : -. ScholarBank@NUS Repository. https://doi.org/10.4050/JAHS.57.012004
dc.identifier.issn00028711
dc.identifier.urihttp://scholarbank.nus.edu.sg/handle/10635/51126
dc.description.abstractA nonlinear flight dynamics model that can be adopted by small-scale unmanned aerial vehicle (UAV) helicopters is presented. To minimize structural complexity, the proposed nonlinear model contains only four essential components, i.e., kinematics, rigid-body dynamics, main rotor flapping dynamics, and yaw rate feedback controller dynamics. A five-step parameter determination procedure is proposed to estimate the unknown parameters of the flight dynamics model. Based on the time-domain evaluations conducted, the nonlinear model is proven to be accurate in capturing the flight dynamics of our UAV helicopter platform over a wide envelope. © 2012 The American Helicopter Society.
dc.description.urihttp://libproxy1.nus.edu.sg/login?url=http://dx.doi.org/10.4050/JAHS.57.012004
dc.sourceScopus
dc.typeConference Paper
dc.contributor.departmentTEMASEK LABORATORIES
dc.contributor.departmentELECTRICAL & COMPUTER ENGINEERING
dc.description.doi10.4050/JAHS.57.012004
dc.description.sourcetitleJournal of the American Helicopter Society
dc.description.volume57
dc.description.issue1
dc.description.page-
dc.description.codenJHESA
dc.identifier.isiut000300326600004
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