Safety is paramount in aviation. To enhance it, we will develop a system for measuring aircraft wing deformations. This will provide engineers with feedback for design and structural improvements, as well as allow us to adjust service intervals. Deformations will be measured using sensors comprising accelerometers and gyroscopes, distributed along the wing. Theoretically, we will determine frequencies and amplitudes of potential disturbances and deformations during flight. Subsequently, we will conduct tests to validate the theoretical scenarios. Throughout the testing phase, we will optimize the system. We have observed that the system performs well in measuring static-type deformations. However, for dynamic-type deformations, some data deviates from reality and needs to be disregarded.
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