- 专利标题: AIRCRAFT CONTROL INPUT DEVICE AND COMMAND INPUT METHOD USING THE SAME
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申请号: US18061042申请日: 2022-12-02
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公开(公告)号: US20230286645A1公开(公告)日: 2023-09-14
- 发明人: Youngshin Kang , Bumjin Park , Seongwook Choi , Yushin Kim , Jongmin Bae , Joowon Choi , Sungho Chang
- 申请人: Korea Aerospace Research Institute
- 申请人地址: KR Daejeon
- 专利权人: Korea Aerospace Research Institute
- 当前专利权人: Korea Aerospace Research Institute
- 当前专利权人地址: KR Daejeon
- 优先权: KR 20210170628 2021.12.02 KR 20220119588 2022.09.21
- 主分类号: B64C13/04
- IPC分类号: B64C13/04 ; B64D43/00
摘要:
The present invention relates to a control input device applicable to an eVTOL aircraft, which is an electric-powered vertical take-off and landing aircraft, and more particularly, to an aircraft control input device that may replace a cyclic control stick, a tail rotor control pedal, and a collective control stick used for flight control of a conventional aircraft, which is simpler in configuration and easier to operate than conventional control devices and may improve pilot convenience and stability of flight operation through simple and accurate flight manipulation, and a command input method using the same.
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