FIELD: aviation.
SUBSTANCE: invention relates to aircraft engineering, namely, to control devices for manned aircrafts (AC) for vertical take-off and landing – multi-copters. Device for controlling manned aircraft vertical takeoff and landing includes two handles – joystick, rigidly fixed on aircraft body, two platforms fixed perpendicular to the sides of the handles by means of metal plates fixed to the platform back sides relative to the pilot and sticks so that the thumbs of the left and right hands of the pilot lay on the stick. At that, in metal plates there are slots allowing to displace platforms for maximum pilot comfort. Two sticks are fixed on front side in the center of platforms relative to pilot on hinges with possibility of deviation in plane of platforms in any direction. Device also includes a toggle switch for emergency disconnection of the device, an on-board flight computer configured to control electric motors of rotors by means of sticks.
EFFECT: facilitating AC control by means of rigidly fixed pilot handles on AC housing, higher stability of pilot position during flight.
1 cl, 2 dwg
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Authors
Dates
2020-06-02—Published
2019-12-06—Filed