Dynamical system structure suitable for vertical take-off and landing aircraft and control method thereof
A power system, vertical take-off and landing technology, applied in the direction of vertical take-off and landing aircraft, aircraft, motor vehicles, etc., can solve problems such as difficult to guarantee stability and reliability, affect the flight quality of level flight, and cannot improve flight efficiency, etc., to achieve control The method is mature and reliable, the effect of good hovering performance in the air and good vertical take-off and landing performance
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[0026] The present invention provides a power system structure suitable for a vertical take-off and landing aircraft, including propellers 61 for providing power. The straight state is tilted upwards to a horizontal state, and the propeller 61 positioned at the rear side of the main wing 2 can be tilted downwards from a vertical state to a horizontal state; The propeller 61 on the rear side of the wing adopts anti-installation to provide thrust and lift for the aircraft; the respective tilting of the propeller 61 on the front and rear sides of the main wing is carried out synchronously; the propeller 61 on the front and rear sides of the main wing is driven by one engine or two The engines are driven separately. The following is a detailed introduction according to the accompanying drawings.
[0027] according to figure 1 , figure 2 As shown, the vertical take-off and landing vehicle of the present invention adopts conventional aerodynamic layout: comprising fuselage 1, ma...
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