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CONTROL METHOD FOR CONTROLLING A YAW ANGLE AND A ROLL ANGLE OF AN AIRCRAFT THAT TAKES OFF VERTICALLY
CONTROL METHOD FOR CONTROLLING A YAW ANGLE AND A ROLL ANGLE OF AN AIRCRAFT THAT TAKES OFF VERTICALLY
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机译:用于控制垂直起飞的横摆角的控制方法和飞机的滚动角度
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摘要
A control method for controlling a yaw angle γz and a roll angle γx of a vertical take-off aircraft comprising at least two drive groups arranged in opposite side regions of the aircraft so as to be spaced apart from a fuselage of the aircraft is presented. Each drive group comprises at least one first drive unit. The first drive unit is arranged so as to be spaced apart from the fuselage to pivot about a pivot angle α into a horizontal flight position and a vertical flight position.
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