Please use this identifier to cite or link to this item: https://hdl.handle.net/10356/64359
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dc.contributor.authorFoo, Faith Inn May
dc.date.accessioned2015-05-26T04:15:48Z
dc.date.available2015-05-26T04:15:48Z
dc.date.copyright2015en_US
dc.date.issued2015
dc.identifier.urihttp://hdl.handle.net/10356/64359
dc.description.abstractThe purpose of this project is to design a UAV that is scalable, with its configuration being dependent on the payload required. Depending on the payload requirements, the UAV can be configured to utilize a variable number of motors, through a “plug-and-play” system. The two designs described in this report achieve scalability differently. The first design (“Prototype 1”) was based on the concept of utilizing multiple identical multi-rotor UAVs mounted on a platform for scalability. The second design (“Prototype 2”) provided scalability by varying the number of rotors on a single UAV, allowing for scalability to be achieved simply without needing an additional platform. The final design (“Final Design”) was based on Prototype 2, with further improvements made to include the implementation of a “plug-and-play” system. This was a major improvement from conventional systems that required the UAV to be re-programmed for each configuration of variable rotor numbers. The construction of both designs will be discussed in this report.en_US
dc.format.extent71 p.en_US
dc.language.isoenen_US
dc.rightsNanyang Technological University
dc.subjectDRNTU::Engineering::Electrical and electronic engineeringen_US
dc.titleDesign considerations of structurally scalable Unmanned Aerial Vehicles (UAV)en_US
dc.typeFinal Year Project (FYP)en_US
dc.contributor.supervisorLim Meng Hioten_US
dc.contributor.schoolSchool of Electrical and Electronic Engineeringen_US
dc.description.degreeBachelor of Engineeringen_US
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Appears in Collections:EEE Student Reports (FYP/IA/PA/PI)
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