Arbitrary Attitude Hovering Control of Quad Tilt Rotor Helicopter | Zendy

Masafumi MIWA | Zendy; Shinji Uemura | Zendy; Akitaka Imamura | Zendy

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Arbitrary Attitude Hovering Control of Quad Tilt Rotor Helicopter

Author(s) -

Masafumi MIWA,

Shinji Uemura,

Akitaka Imamura

Publication year - 2016

Publication title -

journal of robotics and mechatronics

Language(s) - English

Resource type - Journals

SCImago Journal Rank - 0.257

H-Index - 19

eISSN - 1883-8049

pISSN - 0915-3942

DOI - 10.20965/jrm.2016.p0328

Subject(s) - tilt (camera) , rotor (electric) , multirotor , control theory (sociology) , attitude control , thrust , aerodynamics , rotation (mathematics) , aerospace engineering , mechanism (biology) , fixed wing , physics , computer science , engineering , wing , control (management) , structural engineering , mechanical engineering , artificial intelligence , quantum mechanics

[abstFig src='/00280003/08.jpg' width=""300"" text='Arbitrary attitude hovering' ] 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.

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