Article

Drone Detection with Chirp-Pulse Radar Based on Target Fluctuation Models

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  • skinnovation
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Abstract

This paper presents a pulse radar system to detect drones based on a target fluctuation model, specifically the Swerling target model. Because drones are small atypical objects and are mainly composed of non‐conducting materials, their radar cross‐section value is low and fluctuating. Therefore, determining the target fluctuation model and applying a proper integration method are important. The proposed system is herein experimentally verified and the results are discussed. A prototype design of the pulse radar system is based on radar equations. It adopts three different pulse modes and a coherent pulse integration to ensure a high signal‐to‐noise ratio. Outdoor measurements are performed with a prototype radar system to detect Doppler frequencies from both the drone frame and blades. The results indicate that the drone frame and blades are detected within an instrumental maximum range. Additionally, the results show that the drone's frame and blades are close to the Swerling 3 and 4 target models, respectively. By the analysis of the Swerling target models, proper integration methods for detecting drones are verified and can thus contribute to increasing in detectability.

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... На другому етапi знайдемо оцiнкиˆ,ˆ. При цьому оцiнки амплiтуди i початкової фазиˆзнаходяться за формулами (6). ...
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... Radar-Based Detection [48][49][50][51]: Radars are commonly utilized for aircraft detection in military and civil fields, including aviation, and are thus recognized as reliable tools for detecting drones. It transmits radio waves, typically in the microwave range, and analyzes the reflected waves to determine the presence, distance, and speed of objects like aircraft or drones [52]. ...
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... A prototype UAV detection system was developed by KAIST to investigate target fluctuation characteristics [25]. This is a 34.5 GHz chirp-pulse radar using three pulse widths for range ambiguity resolution. ...
... As the optimization process is a task to find a phase matrix S, we selected L, M, and N to constitute the phase matrix S as independent variables, and λ was used for the objective function. The chirp bandwidth and pulse width were fixed to 16 MHz and 1 µs, respectively (the netted radar system for detecting drones normally consists of up to 8 radars and uses the same pulse length of 1 µ to perform the same role [19] and 16 MHz, respectively). The sampling rate used in the MATLAB simulation was set to 256 MHz. ...
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The theoretical return signal from aircraft propeller blades is analyzed. The basic theory involved is described, some simulation results are examined, and some practical considerations are discussed. It is shown that the modulation contained in the return signal is a form of frequency modulation and results in a number of sidebands about the center frequency of the target. It has also been shown that the modulation is due to six main variables, four of which are parameters of the propeller blades, one of which depends on the radar, and one of which depends on the aspect angle of the propeller
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This report considers the probability of detection off a target by a pulsed search radar, when the target has a fluctuating cross section. Formulas for detection probability are derived, and curves off detection probability vs, range are given, for four different target fluctuation models. The investigation shows that, for these fluctuation models, the probability of detection for a fluctuating target is less than that for a non-fluctuating target if the range is sufficiently short, and is greater if the range is sufficiently long. The amount by which the fluctuating and non-fluctuating cases differ depends on the rapidity of fluctuation and on the statistical distribution of the fluctuations. Figure 18, p. 307, shows a comparison between the non-fluctuating case and the four fluctuating cases considered.
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This paper gives a theoretical solution to the problem of determining the electromagnetic backscattering and Doppler spectrum of an aircraft propeller as presented to a radar operating in the 8-12 GHz band. At this band for all practical aircraft propeller the electromagnetic backscattering regime is in the optical region. The solution proceeds by modeling the aircraft propeller as a set of multiple skew-plated metal fan blades in the presence of a linearly polarized EM wave. Based on the quasi-stationary method combined with physical optics and physical theory of diffraction equivalent currents techniques are used to analyse the backscattering from aircraft propeller blades. Experimental results indicated that, in the far zone, the field can be considered as harmonic and expressions for the spectral components of the field are obtained. The observed waveforms are found to be in good agreement with theoretical results
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Analysis of the Effects of Blade Pitch on the Radar Return Signal from Rotating Aircraft Blades
  • J Martin
  • B Mulgrew
J. Martin and B. Mulgrew, "Analysis of the Effects of Blade Pitch on the Radar Return Signal from Rotating Aircraft Blades," Int. Conf. Radar, Oct. 1992, pp. 446-449.
35 GHz FMCW Drone Detection System
  • J Drozdowicz
J. Drozdowicz et al., "35 GHz FMCW Drone Detection System," Int. Radar Symp., Krakow, Poland, May 10-12, 2016, pp. 1-4.
Detection of UAVs Using the MIMO Radar Miracle-KA
  • J Klare
  • O Biallawons
  • D Cerutti-Maori
J. Klare, O. Biallawons, and D. Cerutti-Maori, "Detection of UAVs Using the MIMO Radar Miracle-KA," Proc. EUSAR 2016: Eur. Conf. Synthetic Aperture Radar, Hamburg, Germany, June 6-9, 2016, pp. 1-4.