Education, Science, Technology, Innovation and Life
Open Access
Sign In

The MD effect of a moving UAV's rotor

Download as PDF

DOI: 10.23977/jnca.2024.090101 | Downloads: 1 | Views: 161

Author(s)

Ziting Xu 1, Yingqi Liu 2

Affiliation(s)

1 School of Information and Communication Engineering, University of Electronic Science and Technology of China, Chengdu, 610000, China
2 Houston International Institute, Dalian Maritime University, Dalian, 116026, China

Corresponding Author

Ziting Xu

ABSTRACT

Explosive growth of private drones pose great threat to privacy and safety. Accurately capturing is necessary for regulations. The micro-Doppler (MD) effect is commonly used to identify small unmanned aerial vehicles (UAVs), especially hovering UAVs. This study analyzes the MD effect of UAV rotor blades. It extracts the time-frequency features during radar-based UAV detection using the Short-Time Fourier Transform (STFT). By comparing the MD characteristics of UAVs in hovering and moving states within the same distance unit, as well as the signal difference when the distance unit changes or remains unchanged during the translation process, this paper analyzes in depth the MD characteristics of UAVs in various motion states. The results show that proper tracking of the range unit is necessary to extract the correct MD of a moving target.

KEYWORDS

UAV Detection, MD Effect, Short Time Fourier Transform, moving target

CITE THIS PAPER

Ziting Xu, Yingqi Liu, The MD effect of a moving UAV's rotor. Journal of Network Computing and Applications (2024) Vol. 9: 1-7. DOI: http://dx.doi.org/10.23977/jnca.2024.090101.

REFERENCES

[1] Li Qian. Application and Development Trend of UAV Technology in Military and Civil Fields [J]. Science and Technology Innovation, 2019, (14): 18-20.
[2] Zhang Ying. Exploration of Civilian Drone Invasion of Citizens' Privacy and Security Issues [J]. Journal of Liaoning Police College, 2019, 21(4): 49-53.
[3] Zhou Hanchu, Zhu Yongzhong, Zhang Lingling, et al. Research Progress on Radar Detection Technology for Rotorcraft UAV Targets [J]. Telecommunications Technology, 2024, 64(08): 1335-1345. DOI: 10.20079/j.issn.1001-893x.240320001.
[4] Liu Zhenming. Discrimination of Bird and Rotorcraft UAV Targets by Integrating Micro-Motion and Motion Features [D]. Civil Aviation University of China, 2023. DOI: 10.27627/d.cnki.gzmhy.2023.000038.
[5] Zhang, Y., & Wu, R. (2019). Micro-Doppler Effect Analysis for a Flapping Wing UAV in Forward Flight. IEEE Sensors Journal, 19(2), 598-607.
[6] He Jiaji. Research on Detection and Tracking Technology of Multi-Rotor UAVs Based on micro-Doppler Effect [D]. Harbin Institute of Technology, 2022. DOI: 10.27061/d.cnki.ghgdu.2022.003230.
[7] Li, J., & Chen, V. C. (2018). "Micro-Doppler Effect of a Hovering Rotor Blade with Fluctuating Rotational Speed." IEEE Transactions on Aerospace and Electronic Systems, 54(2), 1111-1125. DOI: 10.1109/TAES.2018.2794163.
[8] Xu, S., & Liu, Y. (2017). "Micro-Doppler Effect Analysis for a Hovering Rotor Blade with Variable Rotational Speed." IEEE Geoscience and Remote Sensing Letters, 14(12), 2336-2340. DOI: 10.1109/LGRS.2017.2755359.
[9] M. Jian, Z. Lu, and V. C. Chen, "Experimental Study of Micro-Doppler Features of UAV Radar," 2017 IEEE Radar Conference (RadarConf), Seattle, WA, USA, 2017, pp. 854-857, doi: 10.1109/radar.2017.7944322.
[10] Lv, Z., Han, S., Peng, L., Yang, L., & Cao, Y. (2022). Weak Fault Feature Extraction of Rolling Bearings Based on Adaptive Variational Modal Decomposition and Multiscale Fuzzy Entropy. Sensors, 22(12), 4504.
[11] C. Bennett, S. Harman, and I. Petrunin, "Realistic Simulation of Drone Micro-Doppler Signatures," 2021 18th European Radar Conference (EuRAD), London, United Kingdom, 2022, pp. 114-117, doi: 10.23919/EuRA D50154. 2022.9784488.
[12] US Patent Application for Signal Detector for Uplink Control Channel and Time Error Correction Method Thereof Patent Application (Application #20140254503 issued September 11, 2014) Justia Patents Search.

Downloads: 1371
Visits: 128832

Sponsors, Associates, and Links


All published work is licensed under a Creative Commons Attribution 4.0 International License.

Copyright © 2016 - 2031 Clausius Scientific Press Inc. All Rights Reserved.