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公开(公告)号：US11809203B2
公开(公告)日：2023-11-07
申请号：US16872825
申请日：2020-05-12
发明人： Youngshin Kang , Am Cho , Seongwook Choi , Yushin Kim , Sung Ho Chang
CPC分类号： G05D1/102 , B64C27/52 , B64C27/82 , G05D1/0858 , B64C2027/8254
摘要： Provided is a vertical take-off/landing aircraft controlling a tilt angle of a main rotor, based on a vertical posture control signal during low-speed flight, wherein, when an aircraft steering signal including a vertical posture control signal for changing the pitch posture angle of the vertical take-off/landing aircraft by a first pitch posture angle is obtained, a flight controller determines a tilt angle of the main rotor with reference to the first pitch posture angle and generates a tilt angle control signal for the main rotor based on the determined tilt angle.
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公开(公告)号：US20230286645A1
公开(公告)日：2023-09-14
申请号：US18061042
申请日：2022-12-02
发明人： Youngshin Kang , Bumjin Park , Seongwook Choi , Yushin Kim , Jongmin Bae , Joowon Choi , Sungho Chang
CPC分类号： B64C13/0421 , B64D43/00 , B64C29/0008
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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