FIELD: measuring equipment.
SUBSTANCE: launch of the unmanned aerial multi-rotor type vehicle (UAV) is performed to the preselected point at the given geographical coordinates and at the desired height. The UAV is transformed to the coordinate holding mode, a uniform motion in vertical, and using the pre-measured empirical relationship, according to the slope of the UAV thrust vector, consumed by the power motors, the speed and direction of wind at the selected point in a vertical section are determined for the atmospheric pressure, the temperature and the air humidity.
EFFECT: expanding the functional capabilities.
1 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| METHOD OF AVERAGE WIND VELOCITY DETERMINATION BY DINT OF UNMANNED AERIAL VEHICLE | 2016 |
|
RU2632270C1 |
| METHOD OF DETERMINING VERTICAL DISTRIBUTIONS OF WIND SPEED AND DIRECTION | 2018 |
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| METHOD FOR DETERMINATION OF AVERAGED VALUES OF WIND SPEED AND DIRECTION | 2015 |
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| METHOD FOR DETERMINING WIND SPEED AND DIRECTION USING UNMANNED AIRCRAFT | 2020 |
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| METHOD FOR DETERMINING HIGHT OF ROUGHNESS OF THE SURFACE OF A RESERVOIR | 2022 |
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RU2634804C2 |
