Fixed-wing unmanned aerial vehicle capable of enhancing pitching control performance of dwelling tail section
A pitch control and fixed-wing technology, applied in rotorcraft, aircraft control, attitude control, etc., can solve problems such as low flight speed, low efficiency of rudder surface execution, and difficulty in pitch attitude control
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[0013] Now in conjunction with embodiment, accompanying drawing, the present invention will be further described:
[0014] In the present invention, a pair of propeller assemblies are installed on the tail of the traditional fixed-wing UAV, and the propeller assemblies include three parts: a small motor installation base, a small brushless motor and blades.
[0015] Two small brushless motors rotate clockwise and counterclockwise respectively, and the motors drive the blades to rotate to generate upward and downward aerodynamic forces respectively. Under the action of the UAV and the moment arm, the UAV generates the head-down moment and the head-up moment respectively. The brushless motor is located on the motor mounting base, and the two brushless motors rotate in opposite directions, thereby offsetting part of the torsional moment generated by the motor rotation, and changing the pulling force of the two propeller assemblies by controlling the speed of the brushless motor. ...
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