A Stake-Out Prototype System Based on GNSS-RTK Technology for Implementing Accurate Vehicle Reliability and Performance Tests
Abstract
:1. Introduction
Geolocalization Applications of GNSS RTK Technology: Architecture and Functionalities of Designed Stake out System
2. Materials and Methods
2.1. GNSS RTK-Based Stake-out Device: Technical Features and Functionalities of Used Components
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- Compass: manufactured by Dioche, it shows the user the cardinal directions to correctly reach the destination points according to FieldGenius indications.
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- Bubble level: it helps the user keep the pole vertical since its inclination can be a positioning error source. The circular bubble level (21.5 mm diameter), manufactured by RS Pro [21], is mounted perpendicular to the pole axis. Its accuracy is 2 mm/m, that is, if the level is oriented parallel to the ground so that the bubble is within the red circle, a deviation error of 2 mm/m from the right plane parallel to the ground is generated. This deviation results in an angular error equal to 0.12° (Figure 7). Being the GNSS antenna positioned 2 m from the pole end in contact with the ground, the positioning error ε due to the bubble level inaccuracy is:ε = l sen(θ) = 4 mm
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- Power bank: a 12 V power bank with 37 Wh capacity powers the VBOX 3iSR INS [22]. The 12 V voltage is supplied by the output connector able to deliver up to 2 A (VBOX 3iSR max absorbed current is 0.625 A corresponding to 7.5 W power [17]). The 37 Wh capacity ensures a 5 h operation of the VBOX 3iSR INS in the case of maximum current absorption [23].
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- GNSS Antenna: model RLACS156 manufactured by Raceologic [24], it is placed on the pole top to obtain a better satellite signals reception (supported frequency band 1574–1606 MHz). According to supplier indication, the antenna (circular with diameter 57 mm) is placed on a metal disk that acts as a ground plane or reflector (diameter 13 cm, thickness 1 cm), with both centers lying on the pole axis [25]. The metal disk redirects the antenna back reception in the frontal direction, improving its gain; however, if it is placed too close to the antenna, the image current produced on the surface can be detrimental to the antenna efficiency [26]. It must be placed a wavelength quarter away from the antenna base so that the back-lobes undergo a 180° phase shift leading to a destructive combination [27].
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- Radio modem: model Satel Satelline-Easy; it allows the VBOX 3iSR INS to receive RTK corrections from the base station (frequency range 403–473 MHz) [28].
2.2. Development of the Matlab Tool for Placing a Set of Points in an Earth Reference System
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- Typing the WGS 84 coordinates (latitude and longitude) of the two points.
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- Choosing two satellite map points by clicking with left/right buttons of the mouse, taking as reference some visible elements of the satellite image (road signs or trees).
3. Results
3.1. Experimental Results of Tests Performed on VBOX 3ISR INS with RLACS156 Antenna
3.2. Automotive Test Preparation on the Testing Track through the Designed Stake-out System
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- Inaccuracies of VBOX 3iSR INS and bubble level of the geolocation device.
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- Distance alterations due to UTM projection.
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- Distance error for i-th point: the difference between the nominal distance and that measured by the Leica 3D Disto sensor, both from the point n. 1 (origin).
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- Percentage distance error for i-th point: the ratio between the distance error and the nominal distance from the point n. 1 (origin).
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- Angular error: the difference between the nominal θ angle (formed by the y-axis and line passing through the points 1 and i-th), measured by the Leica 3D Disto sensor.
4. Discussion
5. Conclusions
Author Contributions
Funding
Institutional Review Board Statement
Informed Consent Statement
Data Availability Statement
Acknowledgments
Conflicts of Interest
References
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VBOX 3iSR with RLACS156 Antenna | |
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Midpoint UTM coordinates | (738504.449 m E; 4466935.146 m N) |
Standard deviation UTM East | 2.3 mm |
Standard deviation UTM North | 3.6 mm |
CEP 95% | 7.5 mm |
Mean | Standard Deviation | Max Value | |
---|---|---|---|
Distance error (cm) | 2.9 | 1.1 | 4.5 |
Percentage distance error % | 0.26 | 0.12 | 0.46 |
Angular error (°) | 0.18 | 0.13 | 0.45 |
Mean | Standard Deviation | Max Value | |
---|---|---|---|
Distance error (cm) | 2.4 | 0.3 | 2.9 |
Percentage distance error % | 0.26 | 0.35 | 0.15 |
Angular error (°) | 0.04 | 0.03 | 0.08 |
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Visconti, P.; Iaia, F.; De Fazio, R.; Giannoccaro, N.I. A Stake-Out Prototype System Based on GNSS-RTK Technology for Implementing Accurate Vehicle Reliability and Performance Tests. Energies 2021, 14, 4885. https://doi.org/10.3390/en14164885
Visconti P, Iaia F, De Fazio R, Giannoccaro NI. A Stake-Out Prototype System Based on GNSS-RTK Technology for Implementing Accurate Vehicle Reliability and Performance Tests. Energies. 2021; 14(16):4885. https://doi.org/10.3390/en14164885
Chicago/Turabian StyleVisconti, Paolo, Francesco Iaia, Roberto De Fazio, and Nicola Ivan Giannoccaro. 2021. "A Stake-Out Prototype System Based on GNSS-RTK Technology for Implementing Accurate Vehicle Reliability and Performance Tests" Energies 14, no. 16: 4885. https://doi.org/10.3390/en14164885
APA StyleVisconti, P., Iaia, F., De Fazio, R., & Giannoccaro, N. I. (2021). A Stake-Out Prototype System Based on GNSS-RTK Technology for Implementing Accurate Vehicle Reliability and Performance Tests. Energies, 14(16), 4885. https://doi.org/10.3390/en14164885