Research on Manipulation Strategy and Flight Test of the Quad Tilt Rotor in Conversion Process
The quad tilt rotor (QTR) has the problem of manipulation redundancy due to the helicopter and fixed-wing manipulation mechanisms. Solving the problem of manipulation redundancy and develop an effective manipulation strategy is critical for QTR during conversion flight. A novel manipulation strategy...
| Main Authors: | , , , , , |
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| Format: | Article |
| Language: | English |
| Published: |
IEEE
2021-01-01
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| Series: | IEEE Access |
| Subjects: | |
| Online Access: | https://ieeexplore.ieee.org/document/9374465/ |
| _version_ | 1818351236008640512 |
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| author | Yonghong Chen Zhigang Wang Zhichao Lyu Jianbo Li Yongwen Yang Yibo Li |
| author_facet | Yonghong Chen Zhigang Wang Zhichao Lyu Jianbo Li Yongwen Yang Yibo Li |
| author_sort | Yonghong Chen |
| collection | DOAJ |
| description | The quad tilt rotor (QTR) has the problem of manipulation redundancy due to the helicopter and fixed-wing manipulation mechanisms. Solving the problem of manipulation redundancy and develop an effective manipulation strategy is critical for QTR during conversion flight. A novel manipulation strategy based on states of QTR is proposed in this paper to solve the problem of manipulation redundancy in conversion mode. The longitude is controlled by the tilt angle of nacelle in helicopter mode and the course is controlled by the speed error of propellers in fixed-wing mode. The Active Disturbance Rejection Control (ADRC) is adopt into the flight control law, which can observe and compensate for internal and external disturbance. The simulation and flight test are carried out to verify the proposed manipulation strategy and the results show that the proposed manipulation strategy is effective and reasonable. |
| first_indexed | 2024-12-13T18:34:31Z |
| format | Article |
| id | doaj.art-016e065dcf344486ba7df6ad8b49cfe1 |
| institution | Directory Open Access Journal |
| issn | 2169-3536 |
| language | English |
| last_indexed | 2024-12-13T18:34:31Z |
| publishDate | 2021-01-01 |
| publisher | IEEE |
| record_format | Article |
| series | IEEE Access |
| spelling | doaj.art-016e065dcf344486ba7df6ad8b49cfe12022-12-21T23:35:24ZengIEEEIEEE Access2169-35362021-01-019402864030710.1109/ACCESS.2021.30650209374465Research on Manipulation Strategy and Flight Test of the Quad Tilt Rotor in Conversion ProcessYonghong Chen0Zhigang Wang1https://orcid.org/0000-0003-1911-5724Zhichao Lyu2Jianbo Li3https://orcid.org/0000-0002-1905-0484Yongwen Yang4Yibo Li5Yangzhou Academy of Collaboration & Innovation Company Ltd., Yangzhou, ChinaYangzhou Academy of Collaboration & Innovation Company Ltd., Yangzhou, ChinaYangzhou Academy of Collaboration & Innovation Company Ltd., Yangzhou, ChinaNational Key Laboratory of Rotorcraft Aeromechanics, Nanjing University of Aeronautics and Astronautics, Nanjing, ChinaYangzhou Academy of Collaboration & Innovation Company Ltd., Yangzhou, ChinaYangzhou Academy of Collaboration & Innovation Company Ltd., Yangzhou, ChinaThe quad tilt rotor (QTR) has the problem of manipulation redundancy due to the helicopter and fixed-wing manipulation mechanisms. Solving the problem of manipulation redundancy and develop an effective manipulation strategy is critical for QTR during conversion flight. A novel manipulation strategy based on states of QTR is proposed in this paper to solve the problem of manipulation redundancy in conversion mode. The longitude is controlled by the tilt angle of nacelle in helicopter mode and the course is controlled by the speed error of propellers in fixed-wing mode. The Active Disturbance Rejection Control (ADRC) is adopt into the flight control law, which can observe and compensate for internal and external disturbance. The simulation and flight test are carried out to verify the proposed manipulation strategy and the results show that the proposed manipulation strategy is effective and reasonable.https://ieeexplore.ieee.org/document/9374465/Quad tilt rotormanipulation redundancymanipulation strategyconversion corridorflight test |
| spellingShingle | Yonghong Chen Zhigang Wang Zhichao Lyu Jianbo Li Yongwen Yang Yibo Li Research on Manipulation Strategy and Flight Test of the Quad Tilt Rotor in Conversion Process IEEE Access Quad tilt rotor manipulation redundancy manipulation strategy conversion corridor flight test |
| title | Research on Manipulation Strategy and Flight Test of the Quad Tilt Rotor in Conversion Process |
| title_full | Research on Manipulation Strategy and Flight Test of the Quad Tilt Rotor in Conversion Process |
| title_fullStr | Research on Manipulation Strategy and Flight Test of the Quad Tilt Rotor in Conversion Process |
| title_full_unstemmed | Research on Manipulation Strategy and Flight Test of the Quad Tilt Rotor in Conversion Process |
| title_short | Research on Manipulation Strategy and Flight Test of the Quad Tilt Rotor in Conversion Process |
| title_sort | research on manipulation strategy and flight test of the quad tilt rotor in conversion process |
| topic | Quad tilt rotor manipulation redundancy manipulation strategy conversion corridor flight test |
| url | https://ieeexplore.ieee.org/document/9374465/ |
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