EXPERIMENTAL CHECKING OF GAS-DYNAMIC METHOD OF UAV LANDING
Journal Title: Електроніка та системи управління - Year 2018, Vol 3, Issue 57
Abstract
In the paper construction of the experimental gas-dynamic stand for checking of the gas-dynamic method of unmanned aerial vehicle landing is developed. Characteristics of this stand were calculated and choose. Series of experiments for given model of unmanned aerial vehicle were conducted. Experiments reveal that at braking of unmanned aerial vehicle into artificial airstream on its motion act next main factors: 1) the angle of attack; 2) uniformity, velocity, and the artificial airstream motion direction. Moreover, obtained results allow more carefully ground requirements to equipment for implement new experiments.
Authors and Affiliations
Nikolay. Tupitsin, Hanna Massalova
Keywords
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- EP ID EP521750
- DOI 10.18372/1990-5548.57.13245
- Views 142
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