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The aerospace wireless sensor network system compatible with microwave power transmission by time- and frequency-division operations

Published online by Cambridge University Press:  24 April 2015

Satoshi Yoshida
Affiliation:
Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency, 3-1-1 Yoshinodai, Chu-oh, Sagamihara 252-5210, Japan. Phone: +81 50 3362 5732
Naoki Hasegawa
Affiliation:
Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency, 3-1-1 Yoshinodai, Chu-oh, Sagamihara 252-5210, Japan. Phone: +81 50 3362 5732 Research Institute for Sustainable Humanosphere, Kyoto University, Gokasho, Uji, Kyoto 611-0011, Japan
Shigeo Kawasaki*
Affiliation:
Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency, 3-1-1 Yoshinodai, Chu-oh, Sagamihara 252-5210, Japan. Phone: +81 50 3362 5732
*
Corresponding author: S. Kawasaki Email: kawasaki.shigeo@jaxa.jp

Abstract

A novel wireless sensor network system with compatibility of microwave power transmission (MPT) using a Gallium Nitride (GaN) power amplifier has been fabricated and tested. The sensor node operates using electrical power supplied by the MPT system. Time- and frequency-division operations are proposed for the compatibility. Under the frequency-division operation, receiving signal strength indicator of −85 dBm and packet error rate of <1% were measured when the available DC power of a rectifier with 160 mW output power. Under 120-min measurement, sustainable power balance between radio-frequency–DC conversion and power consumption in stable operation of the sensor node was achieved.

Information

Type
Research Article
Copyright
Copyright © Cambridge University Press 2015 
Figure 0

Table 1. The type of WPT by power delivery principles.

Figure 1

Table 2. The type of MPT by available transferred power.

Figure 2

Fig. 1. The system block diagrams of the proposed sensor network system compatible with MPT: (a) the time-division operation and (b) the frequency-division operation.

Figure 3

Table 3. Link budget of the 5.8 GHz band wireless communication.

Figure 4

Fig. 2. Measurement condition of the propagation loss using the RVT [35]: (a) locations of the base station and the sensor node and (b) after attachment of the aeroshell.

Figure 5

Table 4. Power diagram of the proposed high power MPT system.

Figure 6

Fig. 3. The scheduling for the time-division operation: (a) the total sequence and (b) the details in one timeslot.

Figure 7

Fig. 4. Variations of the timeslot assignment depending on the communication situations.

Figure 8

Fig. 5. The block diagram of the MPT system evaluation: (a) in the base station and (b) in the sensor node.

Figure 9

Fig. 6. The block diagram of the time-division operation evaluation of the wireless communication in the 5.8 GHz band and the MPT at 5.8 GHz: (a) in the base station and (b) in the sensor node.

Figure 10

Fig. 7. The block diagram of the frequency-division operation evaluation of the wireless communication in the 2.4 GHz band and the MPT at 5.8 GHz: (a) in the base station and (b) in the sensor node.

Figure 11

Fig. 8. The block diagram of the HPA unit.

Figure 12

Fig. 9. The fabricated HPA unit: (a) the driver amplifier, (b) the middle-power amplifier, and (c) the high-power amplifier.

Figure 13

Fig. 10. Measurement results of the input–output characteristics of the HPA unit.

Figure 14

Fig. 11. Measurement results of the optput power spectrum from the HPA unit.

Figure 15

Fig. 12. The photograph of the fabricated 5.8 GHz rectifier.

Figure 16

Fig. 13. Measurement results of the rectifier: (a) the DC output power and (b) the RF–DC conversion efficiency.

Figure 17

Fig. 14. The photograph of the fabricated 2 × 2 rectenna array: (a) the front side and (b) the back side.

Figure 18

Fig. 15. The fabricated 5.8 GHz 4 × 4 circular patch array antenna.

Figure 19

Fig. 16. Measurement results of radiation patterns of the 4 × 4 array antenna.

Figure 20

Fig. 17. Photographs of the fabricated base station and the sensor node: (a) the base station and (b) the sensor node.

Figure 21

Fig. 18. Measurement results of the DC output power and the RF–DC conversion efficiency of the four rectennas.

Figure 22

Fig. 19. Measurement results of the battery charging by the MPT system.

Figure 23

Table 5. Dependence on the communication antenna location for the time-division operation.

Figure 24

Fig. 20. Dependence on antenna distance for the time-division operation: (a) the RSSI, the PER, and the rectifier output power and (b) the drain current of the HPA and rectifier output power.

Figure 25

Table 6. Dependence on the MPT parameters.

Figure 26

Fig. 21. Dependence on antenna distance for the frequency-division operation: (a) the RSSI, the PER, and the rectifier output power and (b) the drain current of the HPA and the rectifier output power.

Figure 27

Fig. 22. Long-time operation measurement results using the frequency-division operation (within 60 min): (a) the voltage and current of the battery and rectifier and (b) the RSSI, the PER, and the rectifier output power.

Figure 28

Fig. 23. Power balance in the sensor node. Conditions A and B mean the rectifier output and the regulator output, respectively.