Please use this identifier to cite or link to this item: https://hdl.handle.net/10356/77975
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dc.contributor.authorTan, Shi Yin
dc.date.accessioned2019-06-10T08:16:15Z
dc.date.available2019-06-10T08:16:15Z
dc.date.issued2019
dc.identifier.urihttp://hdl.handle.net/10356/77975
dc.description.abstractThis report serves to document the development and design process of a fault tolerant Unmanned Aerial Vehicle (UAV), specifically a quadrotor, utilizing the independent command of 2 degree of freedom (DOF) rotation from each propeller. The report details the design of the augmented UAV propeller in which a propeller with two-axes of rotation is implemented in order to achieve control over 2-DoF motion of the propeller. Various design iterations and concepts are also explored and compared. The stress and deformation analysis of each design is also detailed in this report. The report then concludes with the various design improvements that can be considered moving forward in the optimization and refinement process for the fault tolerant UAV.en_US
dc.format.extent67 p.en_US
dc.language.isoenen_US
dc.rightsNanyang Technological University
dc.subjectDRNTU::Engineering::Aeronautical engineeringen_US
dc.titleDesign and analysis of a novel quadrotor with a two-axes propeller rotationen_US
dc.typeFinal Year Project (FYP)en_US
dc.contributor.supervisorTegoeh Tjahjowidodoen_US
dc.contributor.schoolSchool of Mechanical and Aerospace Engineeringen_US
dc.description.degreeBachelor of Engineering (Aerospace Engineering)en_US
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Appears in Collections:MAE Student Reports (FYP/IA/PA/PI)
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Design and Development of a Novel Quadrotor with a Two-Axes Propeller Rotation.pdf
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