Design and analysis of a novel quadrotor with a two-axes propeller rotation
This 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...
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| Format: | Final Year Project |
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2019
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| Online Access: | http://hdl.handle.net/10356/77975 |
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sg-ntu-dr.10356-779752023-03-04T18:53:59Z Design and analysis of a novel quadrotor with a two-axes propeller rotation Tan, Shi Yin Tegoeh Tjahjowidodo School of Mechanical and Aerospace Engineering DRNTU::Engineering::Aeronautical engineering This 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. Bachelor of Engineering (Aerospace Engineering) 2019-06-10T08:16:15Z 2019-06-10T08:16:15Z 2019 Final Year Project (FYP) http://hdl.handle.net/10356/77975 en Nanyang Technological University 67 p. application/pdf |
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Nanyang Technological University |
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NTU Library |
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Asia |
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Singapore Singapore |
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DR-NTU |
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English |
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DRNTU::Engineering::Aeronautical engineering |
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DRNTU::Engineering::Aeronautical engineering Tan, Shi Yin Design and analysis of a novel quadrotor with a two-axes propeller rotation |
| description |
This 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. |
| author2 |
Tegoeh Tjahjowidodo |
| author_facet |
Tegoeh Tjahjowidodo Tan, Shi Yin |
| format |
Final Year Project |
| author |
Tan, Shi Yin |
| author_sort |
Tan, Shi Yin |
| title |
Design and analysis of a novel quadrotor with a two-axes propeller rotation |
| title_short |
Design and analysis of a novel quadrotor with a two-axes propeller rotation |
| title_full |
Design and analysis of a novel quadrotor with a two-axes propeller rotation |
| title_fullStr |
Design and analysis of a novel quadrotor with a two-axes propeller rotation |
| title_full_unstemmed |
Design and analysis of a novel quadrotor with a two-axes propeller rotation |
| title_sort |
design and analysis of a novel quadrotor with a two-axes propeller rotation |
| publishDate |
2019 |
| url |
http://hdl.handle.net/10356/77975 |
| _version_ |
1759857387838111744 |