Affordable Data Collection System for UAVs Taxi Vibration Testing

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Authors: Chaoyi Lin Yang, Gabriele Dessena, Oscar Elías Bonilla-Manrique
Cited by: 0

Abstract

Abstract Structural vibration testing plays a key role in aerospace engineering for evaluating dynamic behaviour, ensuring reliability and verifying structural integrity. These tests rely on accurate and robust data acquisition systems (DAQ) to capture high-quality acceleration data. However, commercial DAQs that provide the required performance and features are often expensive and complex, limiting their accessibility for small-scale research and experimental applications. This work presents the design and experimental validation of an affordable and in-house-developed acceleration DAQ, tested on a small fixed-wing UAV through several Taxi Vibration Test (TVT) runs and ambient vibration measurements. The proposed system integrates three OrangePi 3 LTS single-board computers (SBC) with multiple, up to four per SBC, LSM6DS3TR-C MEMS inertial measurement units operating simultaneously via an Inter-Integrated Circuit (I2C) communication interface, managed under a Python-based master/slave architecture. data are acquired at a stable sampling rate of approximately 208 Hz and post-processed using Welch’s method to estimate their Power Spectral Density (PSD). Results confirm the system ability to provide consistent multi-sensor acceleration data and repeatable PSD profiles under the same test conditions; thus, demonstrating its reliability. With a total hardware cost below €600 (∼$690), the developed DAQ offers a compact, scalable and cost-effective alternative for aerospace vibration analysis and structural testing.

Fields of Study & Subjects

Embedded Systems and FPGA Design Inertial Sensor and Navigation Aeroelasticity and Vibration Control

Publication details

Journal / source
ASME Aerospace Structures, Structural Dynamics, and Materials Conference (SSDM)
Publication date
8 June 2026