Highly-maneuverable quadcopter flight test and autopilot parameters tuning
During the last decade, quadcopter, or quad rotor helicopter, is becoming more and more popular in vertical takeoff and landing (VTOL) unmanned aerial vehicle (UAV) research field due to its high performance in hovering and maneuverability.
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| Format: | Final Year Project (FYP) |
| Language: | English |
| Published: |
2012
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| Online Access: | http://hdl.handle.net/10356/50513 |
| _version_ | 1826115087250751488 |
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| author | Wang, Hao |
| author2 | Go Tiauw Hiong |
| author_facet | Go Tiauw Hiong Wang, Hao |
| author_sort | Wang, Hao |
| collection | NTU |
| description | During the last decade, quadcopter, or quad rotor helicopter, is becoming more and more popular in vertical takeoff and landing (VTOL) unmanned aerial vehicle (UAV) research field due to its high performance in hovering and maneuverability. |
| first_indexed | 2024-10-01T03:49:48Z |
| format | Final Year Project (FYP) |
| id | ntu-10356/50513 |
| institution | Nanyang Technological University |
| language | English |
| last_indexed | 2024-10-01T03:49:48Z |
| publishDate | 2012 |
| record_format | dspace |
| spelling | ntu-10356/505132023-03-04T18:25:44Z Highly-maneuverable quadcopter flight test and autopilot parameters tuning Wang, Hao Go Tiauw Hiong School of Mechanical and Aerospace Engineering DRNTU::Engineering::Aeronautical engineering::Aircraft During the last decade, quadcopter, or quad rotor helicopter, is becoming more and more popular in vertical takeoff and landing (VTOL) unmanned aerial vehicle (UAV) research field due to its high performance in hovering and maneuverability. Bachelor of Engineering (Aerospace Engineering) 2012-06-11T07:40:44Z 2012-06-11T07:40:44Z 2012 2012 Final Year Project (FYP) http://hdl.handle.net/10356/50513 en Nanyang Technological University 57 p. application/pdf |
| spellingShingle | DRNTU::Engineering::Aeronautical engineering::Aircraft Wang, Hao Highly-maneuverable quadcopter flight test and autopilot parameters tuning |
| title | Highly-maneuverable quadcopter flight test and autopilot parameters tuning |
| title_full | Highly-maneuverable quadcopter flight test and autopilot parameters tuning |
| title_fullStr | Highly-maneuverable quadcopter flight test and autopilot parameters tuning |
| title_full_unstemmed | Highly-maneuverable quadcopter flight test and autopilot parameters tuning |
| title_short | Highly-maneuverable quadcopter flight test and autopilot parameters tuning |
| title_sort | highly maneuverable quadcopter flight test and autopilot parameters tuning |
| topic | DRNTU::Engineering::Aeronautical engineering::Aircraft |
| url | http://hdl.handle.net/10356/50513 |
| work_keys_str_mv | AT wanghao highlymaneuverablequadcopterflighttestandautopilotparameterstuning |