4. Optical Fiber Sensors at the Acropolis of Athens
The current section presents the use of optical fibers for structural monitoring at the Acropolis of Athens. Cultural Heritage Sites, such as the Acropolis, are of paramount importance to both national and international heritage, yet they face significant risks, with the potential for irreversible damages. Assessing the structural risks at these sites is a complex and critical task, as they are exposed to various natural and human-made hazards throughout their lifecycle. Effective structural monitoring plays a key role in evaluating these risks and is vital for ensuring the safety of visitors.
The Acropolis, a UNESCO World Heritage site, symbolizes classical civilization and stands atop a rocky Hill about 150 meters above sea level and 70 meters above the city of Athens. The Hill has a trapezoidal shape, measuring roughly 350 meters in length and 150 meters in width, and forms part of the Lycabettus- Tourkovounia-Acropolis ridge complex (
Koukis et al., 2015). Its geology consists of limestone over Athenian schist, with the site surrounded by fortification walls built over 2500 years ago. The Acropolis, despite its historical and cultural importance, has endured considerable damage from both natural hazards and human actions, including wars, invasions, pollution and seismic activity, all of which have progressively increased the risk of structural degradation. Notably, studies have recorded specific seismic events impacting the site, such as those occurring in 1705 and 1805 in Athens, as well as in 1837 in Troezen (
Ambraseys, 2010). Among the standing monuments on the Acropolis hill such as the Parthenon, the Propylea and the Erechtheion, the Perimeter Wall serves a pure geotechnical purpose, since it functions as a typical gravity wall, retaining the backfill that forms the plateau of the Acropolis
The Circuit Wall of the Acropolis Hill is an ancient masonry retaining wall primarily composed of irregular mixed courses of marble and small stones added during subsequent repairs. It spans approximately 800 meters in length and varies in height from 5 to 18 meters.
Figure 16 (left) shows a cross-section of the southern part of the Circuit Wall (left) (
Trikkalinos, 1977) and a panoramic view of the Acropolis Hill, the Circuit Wall, and the Parthenon from the southeast (right).
Aiming to the investigation of the structural integrity of the Acropolis Circuit Wall and Hill, a monitoring scheme with FBG optical fiber sensors has been developed (
Kapogianni et al., 2019). This monitoring system includes eight active optical fiber strain sensors attached every two, one on the inner side and one on the outer side of four smart rods, (noted as IN and OUT, respectively), two temperature sensors, and one acceleration sensor, transmitting real-time, remotely. The smart rods were attached using stainless steel plates anchored to the substrate, allowing them to be easily detached, if necessary, since no adhesive was applied. Optical signal transmission was facilitated by an optical sensing interrogator, and the sensors were connected and spliced in the field in both series and parallel configurations.
Figure 17 highlights the locations of the installed smart rods and the FBG acceleration sensor on the South Wall and at the Acropolis Hill. This specific location of the Circuit Wall was chosen for the optical fiber array installation for several key reasons: a) The South Wall in this area reaches one of its greatest heights (~18 m) along the Circuit Wall and contains a significant volume of backfill material. b) Visible cracks have been detected in this portion of the South Wall, indicating structural vulnerability. c) The selected area is positioned near two pre-existing accelerographs, which form part of the accelerographic network on Acropolis Hill.
Figure 18 displays the strain, temperature and acceleration sensors installed on the Wall, including the anchoring steel plates. The Fiber Bragg Grating single-axis acceleration sensor was positioned perpendicularly to the Wall and integrated into the optical fiber array, connected in both series and parallel with the other sensors as can be seen in
Figure 19. This setup complements an existing monitoring system with 10 high-quality broadband accelerographs positioned strategically across the Acropolis Hill. These devices provide continuous recordings, with 24-bit digitizers transmitting real-time data for ongoing evaluation (
Kalogeras et al., 2010).
For a strain-based optical fiber sensor, the Bragg wavelength shift caused by strain is described by the equation:
where Δε
i is the strain change, Δλ
i the wavelength change,Κε is a ratio expressing the strain-wavelength relation and is equal to 1 .2 picometer (pm)/μstrain for the type of sensors that was used in the current study, Κτ.Δτ
i incorporates the wavelength changes due to the temperature variations. Kτ is equal to 11.2 pm/C
0 for the sensors used in the current study, and Δτ
i is the temperature variation.
In order to convert the wavelength variation to strain the final equation used for the current study is the following: Δεi=Δλi/Κε (3). An example of the calculations is as follows: for λ1=1566.247nm=1566247pm and reference value λ0=1566.064 nm=1566064pm, it is calculated Δλ1 =183 pm and Δε1=183pm/ (1.2 pm/μstrain) =152.5 μstrain.
The relationship between wavelength shifts and acceleration for a single-axis acceleration sensor is determined by the sensor's sensitivity to dynamic forces. The main goal is to measure the shift, Δλ, resulting from applied accelerations. Changes in acceleration cause a corresponding shift in the Bragg wavelength, which is directly proportional to the applied acceleration, as expressed by the following equation (2) and the Single-axis acceleration sensor specifications specifications used in the current study can be seen in
Table 1.
where Δλ
i is the wavelength shift (in pm) from the reference value (average or dataset)S is the sensitivity of the sensor (S=75pm/g for the current study), and a
i is the acceleration (in units of g or m/s
2).
In order to convert the wavelength variation to acceleration the final equation used for the current study is the following:
An example of the calculations is as follows: for λ1=1561.063 nm and reference value λ0=1561.062 nm, it is calculated Δλ1 =0.001nm=1pm and a1= Δλ1/S=0.0133g.
To ensure precise measurements in environments with varying temperatures, it is crucial to account for temperature effects, which can induce wavelength shifts similar to those caused by strain or acceleration. Temperature variations affect the Bragg wavelength through two primary mechanisms: thermal expansion of the optical fiber, which alters the grating spacing, and changes in the refractive index of the material. These temperature-induced shifts are unrelated to strain or acceleration and must be decoupled to ensure accurate measurements.
For strain sensors, a temperature sensor placed near the strain sensors allows the temperature-induced shift to be quantified and subtracted from the total wavelength shift. This isolates the strain-induced wavelength shift, providing accurate strain measurements. Similarly, in single-axis acceleration sensors, the same temperature-induced effects must be accounted for using the sensor’s temperature coefficient (in nm/°C). By incorporating this coefficient, the temperature effects can be corrected, isolating the acceleration-induced wavelength shift for precise acceleration measurement.
The total observed wavelength shift, Δλ_total, is the combined result of both strain and temperature effects and is expressed by the following relationship:
where Δλ
total is the measured total wavelength shift, Δλ
strain is the is the component due to strain and Δλ
temperature is the component due to temperature changes. By subtracting Δλ
temperature from Δλ
total , the strain-induced wavelength shift can be accurately isolated, ensuring precise measurement of strain.
The following figures illustrate strain, acceleration, and temperature recordings from the Circuit Wall of the Acropolis of Athens. An initial analysis investigates the effect of temperature on strain measurements. Specifically,
Figure 20 compares strain data with and without thermal compensation for sensors No. 1 and No. 4, positioned both at the locations labeled IN and OUT. The findings show that strain values are higher when temperature effects are not compensated for, as expected. This increase in strain values can be attributed to the sensitivity of optical fiber sensors to temperature fluctuations. As aforementioned, in optical fiber strain sensors, such as those based on Fiber Bragg Grating, temperature changes can induce shifts in the fiber’s refractive index and grating spacing, which are misinterpreted as strain. Without compensation for these temperature-induced shifts, the total observed wavelength shift includes both strain and thermal effects, leading to inflated strain measurements. Implementing thermal compensation allows for the isolation of strain-induced wavelength shifts, ensuring that the measurements accurately reflect the mechanical deformation of the structure.
Figure 21 depict a comparison of strain variation at the IN and OUT positions for the same smart rods. It is observed that for sensor No. 1, the variation between the inner and outer sensors is minimal, whereas for sensor No. 4, the corresponding variation is significantly larger for the sensor located at the position OUT. It should be noted that the data presented show measurements following thermal compensation. The difference in strain variation between sensors No. 1 and No. 4 could be attributed to several factors such as position and environmental exposure, structural factors, sensor sensibility or calibration, boundary conditions and load distribution. The overall study shows that No. 4 is positioned in an area more exposed to environmental stressors or thermal gradients compared to sensor No 1, leading to higher strain differences. Furthermore, variations in material properties or localized stress concentrations in the rod could result in more pronounced strain differences at specific positions. Finally, sensor No. 4 might exhibit a higher sensitivity to strain or a slight discrepancy in calibration compared to sensor No. 1, amplifying the observed variation.
Figure 22. illustrates the strain variation for four sensors placed on the four smart rods at both IN and OUT positions, with thermal compensation applied. As observed, for the sensors at the OUT positions, the highest strains are recorded by sensor No. 4, while the lowest strains are noted by sensor No. 1. Conversely, for the sensors at the IN positions, sensor No. 2 exhibits the highest strains, while sensor No. 4 shows the lowest. This pattern aligns with previous observations, where sensor No. 4 at the OUT position experiences the greatest strain variation. The differences can be explained by the varying exposure of the sensors to temperature gradients, structural properties, or external forces at different positions. Sensor No. 4, located at the OUT position, is likely subjected to more significant environmental or mechanical influences, resulting in higher strain, whereas sensor No. 1 at the same position is less affected. Meanwhile, sensor No. 2 at the IN position may be more sensitive to temperature-induced strain or other localized effects, contributing to the higher readings observed.
The following figures present the acceleration levels recorded by the single-axis acceleration sensor over the same time period.
Figure 23 (left) examines the impact of temperature on the measurements, revealing a significant effect. As observed, the acceleration values
) recorded show opposite directions—positive without thermal compensation and negative with compensation—indicating that the results would have been substantially different in the absence of thermal compensation.
Figure 22 (right) illustrates the temperature variation recorded by the two temperature sensors (IN and OUT positions, respectively). When thermal compensation is not applied, temperature-induced changes—such as expansion or contraction of the sensor materials or shifts in the sensor's characteristics (e.g., refractive index, grating spacing in fiber sensors)—can introduce false readings. These temperature effects can cause the acceleration values to appear in the opposite direction (positive without compensation and negative with compensation), as thermal expansion or contraction may alter the sensor's measurements in a way that mimics or counteracts the actual acceleration.
The following figures compare acceleration levels
with and without thermal compensation, using the average/mean wavelength measured during this time period as the reference wavelength, instead of the initial measurement used in the previous figures. In this case, the difference between the acceleration values with and without thermal compensation is smaller. Additionally,
Figure 24 compares accelerations calculated using the mean wavelength as the reference with those calculated using the initial wavelength, including thermal compensation. As observed, the peak acceleration values are lower when the mean wavelength is used. However, the overall pattern of acceleration variation (i.e., increases/decreases and higher/lower values) remains similar in both cases.
The smaller difference in acceleration values with and without thermal compensation, when using the mean wavelength as the reference, occurs because the mean wavelength likely reflects a more stable, averaged condition over the measurement period, reducing the impact of short-term temperature fluctuations. When the mean wavelength is used, the sensor’s response to temperature-induced shifts is effectively averaged out, which minimizes the discrepancies between the compensated and non-compensated readings. This leads to more consistent acceleration values regardless of the thermal compensation. In contrast, using the initial wavelength as the reference may result in larger variations because it represents a snapshot at a specific time, which could be more sensitive to temperature changes or other environmental factors. The peak acceleration values are lower with the mean wavelength due to the smoothing effect of averaging, but the overall trend in acceleration variation remains similar, as the underlying acceleration dynamics have not changed; only the reference point for measurement has shifted.