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Miniature drone antenna design for the detection of airliners

Published online by Cambridge University Press:  14 July 2020

Alassane Sidibe*
Affiliation:
LAAS-CNRS, Université de Toulouse, CNRS, UPS, 7, Avenue du Colonel Roche, 31400 Toulouse, France Uwinloc, 9, Rue Humbert Tomatis, 31200 Blagnac, France
Gaël Loubet
Affiliation:
LAAS-CNRS, Université de Toulouse, CNRS, UPS, 7, Avenue du Colonel Roche, 31400 Toulouse, France
Alexandru Takacs
Affiliation:
LAAS-CNRS, Université de Toulouse, CNRS, UPS, 7, Avenue du Colonel Roche, 31400 Toulouse, France
Guillaume Ferré
Affiliation:
IMS Laboratory, Université de Bordeaux-IPB ENSEIRB-MATMECA, 351, cours de la libération, 33400 Talence, France
Anthony Ghiotto
Affiliation:
IMS Laboratory, Université de Bordeaux-IPB ENSEIRB-MATMECA, 351, cours de la libération, 33400 Talence, France
*
Author for correspondence: Alassane Sidibe, E-mail: asidibe@laas.fr
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Abstract

In this paper, the design of a miniature antenna dedicated to the detection of airliners through the demodulation of Automatic Dependence Surveillance-Broadcast system (ADS-B) signals is presented. This antenna is designed for being embedded on the top of a drone in order to detect and avoid collisions with airliners. This antenna consists of an array of Planar Inverted-F Antennas, a quadrature feed network (FN) and a reflector plane (RP). The FN is designed to have output signals with the same amplitude and a 90° phase difference between each other. It achieves circular polarization and maintains the axial ratio of the antenna under −3 dB at the desired frequency (1.09 GHz). The antenna with the FN was manufactured and characterized. It weighs approximately 145 kg with its RP. The measured gain of the proposed antenna is about +3.7 dBi. To validate the design, the manufactured antenna was tested with a Universal Software Radio Peripheral for the processing of ADS-B signals at the French National Microwaves Days 2019 (JNM) student contest. The detection of airliners can reach up to 437 km.

Information

Type
IJMWT Special Issue on the 2019 National Microwave Days
Copyright
Copyright © Cambridge University Press and the European Microwave Association 2020
Figure 0

Fig. 1. Configuration of the antenna with single PIFA.

Figure 1

Table 1. Geometrical parameters of a single PIFA antenna

Figure 2

Fig. 2. (a) Simulated reflection coefficient and (b) radiated pattern of a single PIFA antenna (xOz/φ = 0° cut – blue solid line – and yOz/φ = 90° – orange dash line –).

Figure 3

Fig. 3. Isometric and bottom view of the array PIFA antenna.

Figure 4

Fig. 4. (a) Simulated reflection coefficient at each port of the antenna; (b) the radiation pattern of the PIFA antenna array in two vertical planes: xOz/φ = 0° (blue solid line) and yOz/φ = 90° (orange dash line).

Figure 5

Fig. 5. (a) Variation of the axial ratio as function of the antenna rotation angle at φ = 0° and 1.09 GHz; (b) antenna rotation angle with the respect to the reflector.

Figure 6

Fig. 6. Circuit model of the feed network.

Figure 7

Fig. 7. Layout and photograph of the fabricated quadrature feed network.

Figure 8

Fig. 8. (a) Simulated (line) and measured (dashed line) of the reflection coefficient (at the input of the feed port); (b) The phase delay between port 1 and each of the others.

Figure 9

Table 2. Measured power split and phase at each port of the feed network at 1.09 GHz

Figure 10

Table 3. Measured phase difference between output ports of the feed network at 1.09 GHz

Figure 11

Fig. 9. (a) Designed antenna on HFSS Software; (b) Photograph of the manufactured antenna.

Figure 12

Fig. 10. (a) Measured (dashed line) and simulated (continuous line) reflection coefficient at the input of the feed port of the PIFA array; (b) the simulated (continuous line) and measured (dashed line) gain for three vertical cut planes (φ = 0°, φ = 45°, and φ = 90°).

Figure 13

Fig. 11. Real-time trajectory on the map of the detected aircraft and a photo of the antenna during tests at the contest.