Prediction method for aerial spray drift of helicopter based on model
A prediction method and helicopter technology, applied in special data processing applications, instruments, electrical digital data processing, etc., can solve problems such as no aerial spraying drift model.
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[0036] In this embodiment, the length of the airfoil section section of the helicopter is L=1200mm; the chord length of the blade is C=140mm; the installation angle of the blade (at r=0.2m) a min =2.4°, a max =12.1°, the total torque can be adjusted from 0% to 99%, and the total working moment is 50%; the torsion angle of the root section of the airfoil section is 9.05°, and the torsion angle of the wing tip section of the airfoil section is 3.05°.
[0037] The model-based method for predicting the drift of spraying pesticides by helicopter in this embodiment comprises the following steps:
[0038] The first step is to simulate the helicopter—measure the surface parameters of the spraying helicopter fuselage, input them into the computer, perform grid processing, and generate a fuselage grid map.
[0039] In the present embodiment, at first the present invention generates a curved surface to the fuselage of the helicopter measured before the first step is performed, and the s...
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