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dc.contributor.authorPi, ChenHuanen_US
dc.contributor.authorLin, JinKwanen_US
dc.contributor.authorCheng, Stoneen_US
dc.date.accessioned2019-04-02T06:04:22Z-
dc.date.available2019-04-02T06:04:22Z-
dc.date.issued2018-01-01en_US
dc.identifier.issn2261-236Xen_US
dc.identifier.urihttp://dx.doi.org/10.1051/matecconf/201815104004en_US
dc.identifier.urihttp://hdl.handle.net/11536/150960-
dc.description.abstractA quadcopter is equipped with four additional jet thrusters on its horizontal plane and vertical to each other in order to improve the maneuverability and positioning accuracy of quadcopter. A dynamic model of the quadcopter with jet thrusters is derived and two controllers are implemented in simulation, one is a dual loop state feedback controller for pose control and another is an auxiliary jet thruster controller for accurate positioning. Step response simulations showed that the jet thruster can control the quadcopter with less overshoot compared to the conventional one. Over 10s loiter simulation with disturbance, the quadcopter with jet thruster decrease 85% of RMS error of horizontal disturbance compared to a conventional quadcopter with only a dual loop state feedback controller. The jet thruster controller shows the possibility for further accurate in the field of quadcopter positioning.en_US
dc.language.isoen_USen_US
dc.titleHigh Accuracy Positioning using Jet Thrusters for Quadcopteren_US
dc.typeProceedings Paperen_US
dc.identifier.doi10.1051/matecconf/201815104004en_US
dc.identifier.journal2017 ASIA CONFERENCE ON MECHANICAL AND AEROSPACE ENGINEERING (ACMAE 2017)en_US
dc.citation.volume151en_US
dc.contributor.department機械工程學系zh_TW
dc.contributor.departmentDepartment of Mechanical Engineeringen_US
dc.identifier.wosnumberWOS:000455190800019en_US
dc.citation.woscount0en_US
Appears in Collections:Conferences Paper