Arbitrary Attitude Hovering Control of Quad Tilt Rotor Helicopter
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- Miwa Masafumi
- Institute of Science and Technology, Tokushima University
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- Uemura Shinji
- Graduate School of Advanced Technology and Science, Tokushima University
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- Imamura Akitaka
- Department of Electronics, Information and Communication Engineering, Osaka Sangyo University
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Description
<p>The quad tilt rotor helicopter (QTRH), a tilt-rotor aircraft prototype, has fixed wings for long-range high-speed flight. Its rotor-tilt mechanism controls 4 rotor-tilt angles independently and controls its roll and pitch angles similarly to a multirotor helicopter. It controls yaw angle by thrust vectoring and moves forward and backward by tilting its rotors. Rotor-tilting maneuvers are the initial stage of flight-mode transition between helicopter and fixed-wing modes.</p>
Journal
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- Journal of Robotics and Mechatronics
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Journal of Robotics and Mechatronics 28 (3), 328-333, 2016-06-20
Fuji Technology Press Ltd.
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Details 詳細情報について
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- CRID
- 1390001288149480320
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- NII Article ID
- 130007671067
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- NII Book ID
- AA10809998
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- ISSN
- 18838049
- 09153942
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- NDL BIB ID
- 027568427
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- Text Lang
- en
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- Data Source
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- JaLC
- NDL Search
- Crossref
- CiNii Articles
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- Abstract License Flag
- Disallowed