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Development of the flight laboratory for research of aerodynamic surfaces deformation
Author(s) -
A. Yu. Poroykov,
D A Surkov,
N. S. Ilina,
S. V. Lebedev,
D. V. Ulyanov,
K M Lapitsky,
E. V. Shmatko
Publication year - 2020
Publication title -
journal of physics. conference series
Language(s) - English
Resource type - Journals
SCImago Journal Rank - 0.21
H-Index - 85
eISSN - 1742-6596
pISSN - 1742-6588
DOI - 10.1088/1742-6596/1636/1/012029
Subject(s) - aerodynamics , aerospace engineering , flight test , flight simulator , airplane , flight dynamics , computer science , simulation , fly by wire , deformation (meteorology) , engineering , wing , automotive engineering , aeronautics , mechanical engineering , physics , meteorology
In-flight measurements are developing directions of aircraft testing. The practical implementation of these tests allows accelerating the development of new types of aircraft, the in-flight tests of serial samples, and their commissioning. Carrying out such tests is associated with high cost. In this paper the creation of a flight laboratory based on an unmanned vehicle is proposed. This will significantly reduce the cost of testing but in-flight conditions will be close to real tests. A system for recording experimental images during in-flight test was developed for conducting studies of deformations of aerodynamic surfaces. In this paper, the system based on single board computer is described; its main functions and features are considered. The results of laboratory tests of the developed system on a model of a deformable wing are presented.

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