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dc.contributor.authorAndersen, Tom Stian
dc.contributor.authorKristiansen, Raymond
dc.date.accessioned2018-03-13T09:14:08Z
dc.date.available2018-03-13T09:14:08Z
dc.date.embargoEndDate2019-07-27
dc.date.issued2017-07-27
dc.description.abstractThis paper addresses the problem of trajectory tracking for underactuated quadrotors. A quaternion based guidance law is proposed which feeds into an attitude control system based on a PD+ control law. The desired attitude from the guidance law is defined such that the attitude control system tries to align the position error along the axis of the translational actuator. Simulation results are provided and discussed to demonstrate the proposed method.en_US
dc.descriptionEmbargoed OA, manuscript version after 24 months from publishing date. Link to publishers version: <a href:http://doi.org/10.1109/ICUAS.2017.7991509>http://doi.org/10.1109/ICUAS.2017.7991509</a>en_US
dc.identifier.citationAndersen TS, Kristiansen R: Quaternion guidance and control of quadrotor. In: Proceedings IEEE International Conference on Unmanned Aircraft Systems, 2017. p. 1597-1601en_US
dc.identifier.isbn978-1-5090-4495-5
dc.identifier.otherFRIDAID 1568110
dc.identifier.other10.1109/ICUAS.2017.7991509
dc.identifier.urihttps://hdl.handle.net/10037/12304
dc.language.isoengen_US
dc.publisherInstitute of Electrical and Electronics Engineers (IEEE)en_US
dc.rights.accessRightsembargoedAccessen_US
dc.subjectVDP::Technology: 500::Electrotechnical disciplines: 540en_US
dc.titleQuaternion guidance and control of quadrotoren_US
dc.typePeer revieweden_US
dc.typeKonferansebidragno
dc.typeBokkapittelno
dc.typeConference objecten_US
dc.typeChapteren_US


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