Meas. Sci. Technol. 8 (1997) 355–375. Printed in the UK PII: S0957-0233(97)72999-0
REVIEW ARTICLE
In-fibre Bragg grating sensors
Yun-Jiang Rao
Applied Optics Group, Physics Department, University of Kent at Canterbury,
Kent CT2 7NR, UK
Received 12 August 1996, in final form 22 October 1996, accepted for publication
21 November 1996
Abstract. In-fibre Bragg grating (FBG) sensors are one of the most exciting
developments in the field of optical fibre sensors in recent years. Compared with
conventional fibre-optic sensors, FBG sensors have a number of distinguishing
advantages. Significant progress has been made in applications to strain and
temperature measurements. FBG sensors prove to be one of the most promising
candidates for fibre-optic smart structures. This article presents a comprehensive
and systematic overview of FBG sensor technology regarding many aspects
including sensing principles, properties, fabrication, interrogation and multiplexing
of FBG sensors. It is anticipated that FBG sensor systems will be commercialized
and widely applied in practice in the near future due to the maturity of economical
production of FBGs and the availability of cost effective interrogation and
multiplexing techniques.
Yun-Jiang Rao was born in
Yunnan, China. He received
his MEng and PhD degrees
in Optoelectronics at the Uni-
versity of Chongqing, China,
in 1986 and 1990. In 1988 he
was employed as a lecturer at
the University of Chongqing,
where he led a research
team to develop the first
fully automatic single-mode
fibre arc-fusion splicing ma-
chine in China. From 1991
to 1992 he worked on all-
fibre optically-addressed sil-
icon microresonator sensors
as a Postdoctoral Research Fellow at the University of
Strathclyde in Scotland. In 1992 he joined the Department
of Physics at the University of Kent at Canterbury as a
Research Fellow, where he has been working on fibre-optic
low coherence interferometry, development of fibre-optic
pressure and temperature sensors, advanced fibre-optic
sensor multiplexing techniques and in-fibre Bragg grating
sensors. He has developed a universal fibre-optic point
sensor system for quasi-static absolute measurements of
multiparameters based on low-coherence interrogation. His
current research interests are intrinsic and extrinsic single-
mode fibre-based sensors, multiplexing techniques, fibre-
optic interferometry and in-fibre grating sensors. He has
authored or co-authored over 30 journal and 40 conference
papers.
1. Introduction
The formation of photogenerated gratings in germanosil-
icate optical fibre by sustained exposure of the core to
the interference pattern produced by oppositely propagat-
ing modes of argon-ion laser radiation was first reported
in 1978 (Hill et al 1978). However, pioneering work at
the United Technology Research Centre, which is regarded
as a milestone for in-fibre Bragg grating (FBG) sensors,
was published eleven years later (Meltz et al 1989). This
side-writing technique creates a Bragg grating directly in
the fibre core using a holographic interferometer illumi-
nated with a coherent ultraviolet source. Versatility in the
fabrication of FBGs has been gained from the fact that
the Bragg wavelength is independent of the writing laser
used. Subsequent to this initial work interest in FBGs has
increased considerably in recent years. There are two prob-
able main reasons for this: (1) the FBG has become a key
passive device for applications in optical fibre telecommu-
nications (Mizrahi 1993), including wavelength-division-
multiplexing, fibre laser and amplifier pump reflectors (Ball
and Morey 1992, Farries et al 1992), gain flattening devices
(Kashyap et al 1993), and dispersion compensation ele-
ments (Ouellette 1991, Williams et al 1994); (2) it has been
demonstrated that FBGs have great potential for a wide
range of sensing applications where quasi-distributed mea-
surements for important physical quantities, such as strain,
temperature, pressure, ultrasound, acceleration, high mag-
netic field and force, are required (Morey et al 1989, 1992,
Xu et al 1993b, Foote et al 1996, Kersey and Marrone
1994, Rao et al 1996f, Webb et al 1996, Theriault et al
1996, Bjerkan et al 1996).
Compared with other implementations of fibre-optic
sensors, FBG sensors have a number of distinguishing
advantages. (1) They can give an absolute measurement
that is insensitive to fluctuations in the irradiance of
the illuminating source, as the information is usually
0957-0233/97/040355+21$19.50 c© 1997 IOP Publishing Ltd 355
Yun-Jiang Rao
obtained by detecting the wavelength shift induced by
the measurand. (2) They can be directly written
into the fibre without changing the fibre diameter,
making them compatible with a wide range of situations
where small diameter probes are essential, such as
in advanced composite materials for strain mapping,
or the human body for temperature profiling. (3)
They can be mass produced at low cost, making them
potentially competitive with conventional electrical sensors
(Askins et al 1994). (4) They can be multiplexed
using similar techniques that have been applied for use
with fibre-optic sensors, including wavelength-division-
multiplexing (WDM), spatial-division-multiplexing (SDM),
time-division-multiplexing (TDM), and their combinations
(Kersey 1993, Rao and Jackson 1996a), making quasi-
distributed sensing feasible in practice. One of the most
important applications of FBG sensors that has been
demonstrated to date is for the so-called ‘fibre-optic smart
structures’, where FBGs are embedded into the structure to
monitor its strain distribution (Udd 1995). Fibre-optic smart
structure technology could in the future lead to structures
that are self-monitoring and even self-scheduling of their
maintenance and repair by the marriage of fibre-optic sensor
technology and artificial intelligence with material science
and structural engineering. In order to see the significance
of FBG sensors, a comparison between FBG sensors and
other fibre-optic strain sensors is given in table 1. It can
be seen that FBG sensors have more advantages than other
fibre-optic strain sensors, making them ideal for fibre-optic
smart structures. However, temperature compensation of
the strain error caused by thermal fluctuation is essential
for practical applications and this issue will be discussed
later.
The aim of this article is to give a comprehensive
and systematic overview of FBG sensor technology in six
sections. Following the introduction, the sensing principles
and properties of FBG sensors are provided in section 2.
In section 3, various fabrication techniques for FBGs are
outlined which make the low-cost mass production of FBGs
feasible. Section 4 deals with a range of interrogation
techniques for FBG sensors, which can achieve high-
resolution wavelength-shift detection. A wide variety of
multiplexing techniques that have been applied to FBG
sensors are discussed in section 5. This article concludes
in section 6 with a summary and discussion of likely future
developments in FBG sensor technology.
2. Principles and properties of FBG sensors
2.1. Optical theory of in-fibre Bragg gratings
An FBG is written into a segment of Ge-doped single-
mode fibre in which a periodic modulation of the core
refractive index is formed by exposure to a spatial pattern
of ultraviolet light in the region of 244–248 nm, as
shown in figure 1. This fabrication process is based on
the photorefractive effect in the germania oxygen-vacancy
defect band, which was observed in Ge-doped optical fibres
by Hill et al (1978). The lengths of FBGs are normally
within the region of 1–20 mm and grating reflectivities
Table 1. Comparison of fibre-optic strain sensors.
FBG FP TM PM
Linear response yes yes.1/ yes.1/ yes.1/
Absolute measurement yes yes.2/ yes.2/ yes.2/
Range to resolution high high low low
Sensor gauge length short short long long
Mechanical strength high low.3/ high high
Multiplexing yes yes.4/ yes.4/ yes.4/
Mass production yes yes.5/ yes.5/ yes.5/
Potential cost low low.6/ low.6/ low.6/
FP: Fabry–Pe´rot interferometric sensors (Kersey et al
1983, Lee et al 1992, Kist et al 1984, Claus et al 1993).
TW: two-mode fibre-optic sensors (Blake et al 1987, Lu
and Blaha 1992).
PM: polarimetric fibre-optic sensors (Varnham et al 1983,
Bock and Wolinski 1991).
.1/ Requires quadrature signal demodulation and it is
difficult to achieve high stability in practice.
.2/ Requires suitable signal processing, such as
low-coherence interferometry (Rao and Jackson 1996c).
.3/ Except for in-line fibre etalon strain sensors (Sirkis et al
1993).
.4/ Difficult if the number of sensors is large, unless
spatial-division-multiplexing is used.
.5/ Requires some handling work either for cavity
construction or for lead-in/lead-out fibre splicing, except
for intrinsic Fabry–Pe´rot sensors made from two FBGs
reported recently (Morey et al 1991).
.6/ Good skills for fibre splicing or sensor assembly are
needed.
Figure 1. Schematic diagram of in-fibre Bragg grating.
can approach �100%. When the FBG is illuminated by
a broadband light source, a set of beams reflected from
a set of partially reflecting planes formed by the periodic
core index modulation interfere with each other. The
interference is destructive unless each beam is in phase with
all the others. According to Bragg’s law which gives this
condition, only one wavelength, i.e. the Bragg wavelength
�B , is selected, which is given by
�B D 2n3 (1)
where n is the effective core index of refraction and 3 the
period of the index modulation.
The reflectivity at the Bragg wavelength can be
estimated using the equation (Lam and Garside 1981)
R D tanh2 (2)
356
In-fibre grating sensors
where
D �n.L=�B/.1n=n/�.V /: (3)
The factor �.V / ’ 1−1=V 2, V � 2:4 is the fraction of the
integrated fundamental mode intensity contained in the core
(V is the normalized frequency of the fibre). It is seen that
R is directly proportional to the grating length L and the
index perturbation (1n=n) which is normally determined
by the exposure power and time of the UV radiation for a
specified fibre.
The full width half maximum (FWHM) bandwidth, 1�,
of a grating is approximately given by (Russell et al 1993)
1� D �Bs
s�
1n
2n
�2
C
�
1
N
�2
(4)
where s � 1 for strong gratings (near 100% reflection) and
s � 0:5 for weak gratings, and N is the number of grating
planes. Because the change in the index is small, the main
contribution to the linewidth change is attributed to the
change in the modulation depth of the index perturbation.
Unlike conventional fibre-optic interferometric sensors
illuminated by highly coherent lasers, FBG sensors
generally require a broadband light source and a high-
resolution wavelength-shift detection system, which will
be discussed later. From the light source point of view,
a wide wavelength bandwidth and high optical power is
normally required to achieve a large range to resolution for
the wavelength shift induced by the measurand. Most of
the sources that have been used for FBG sensors are similar
to those used for fibre-optic gyroscopes and low-coherence
interferometric sensors (Lefevre 1993, Jackson 1994).
They include edge-emitting light emitting diodes (ELEDs),
superluminescent diodes (SLDs), superflourescent fibre
sources (SFSs) and tuneable fibre lasers (TFLs). Table 2
gives a comparison of these sources.
2.2. Sensing principles
FBG sensors have been reported for measurements of strain,
temperature, pressure, dynamic magnetic field, etc. The
FBG central wavelength will vary with the change of these
parameters experienced by the fibre and the corresponding
wavelength shifts are as follows.
2:2:1. Strain. The wavelength shift, 1�BS , for an applied
longitudinal strain 1" is given by
1�BS D �B.1− ��/1" (5)
where �� is the photoelastic coefficient of the fibre, given
by
�� D n
2
2
[�12 − �.�11 − �12/] (6)
where �11 and �12 are the components of the fibre-optic
strain tensor and � is Poisson’s ratio. For the silica
fibre, the wavelength–strain sensitivities of 800 nm and
1.55 �m FBGs have been measured as � 0:64 pm �"−1 and
� 1:15 pm �"−1 respectively (Morey et al 1989, Rao et al
1995b). For the measurement of acceleration, ultrasound
Figure 2. Linearly chirped FBG sensor.
and force, equations (5) and (6) are still applicable as these
measurands are converted from strain.
Linearly chirped FBGs have been demonstrated as
dispersion compensation elements for high-speed optical
fibre communication systems (Ouellette 1991, Williams
et al 1994). These devices act as a wavelength bandpass
filter in which the pitch of the grating is varied along the
position of the grating length and the chirped FBG reflects a
large number of wavelengths, i.e. optical frequencies, from
different positions of the grating, as shown in figure 2. The
principle of using this chirped device for strain sensing is
based on the effective change in reflection point, �b, which
is given by (Kersey and Davis 1994)
�b D − �
1�C
B�1" (7)
where � is a constant determined by the photoelastic
properties of the fibre and B is the grating length. � is
a fixed source wavelength and 1�C D �B1 − �B2 with
�B1 < �B2 (see figure 2). For comparison, the optical
length change for a length of fibre B is given by
�l D B�1": (8)
The ratio of equations (7) and (8) is thus expressed in the
form
�b
�l
D − �
1�C
: (9)
It can be seen that because � � ��C; �b � �l, hence
the chirped FBG gives a very large strain transduction
amplification factor. From the high-sensitivity point of
view, linearly chirped FBGs have potential advantages
for dynamic strain measurement. Another potential use
of chirped FBGs is for distributed strain measurement by
sequentially interrogating short sections along the grating
with low-coherence interferometry (Volanthen et al 1996).
2:2:2. Temperature. For a temperature change of 1T ,
the corresponding wavelength shift 1�BT is given by
1�BT D �B.1C �/1T (10)
where � is the fibre thermo-optic coefficient. For the silica
fibre, the wavelength–temperature sensitivities of 800 nm
357
Yun-Jiang Rao
Table 2. Comparison of light sources for FBG sensors.
ELEDs SLDs SFSs TFLs
Optical power� 1–10 �W 0.1–2 mW 1–10 mW 0.1–10 mW
FWHM bandwidth 40–100 nm 15–30 nm 20–40 nm 1–10 nm��
Device cost low medium high high
� Optical power coupled into single-mode fibre.
�� Tuneable wavelength range.
Table 3. Strain and temperature sensitivities of FBG
sensors with different wavelengths.
Wavelength Strain sensitivity Temperature sensitivity
(�m) (pm �"−1) (pm �C−1)
0.83 �0.64 �6.8
1.3 �1 �10
1.55 �1.2 �13
and 1.55 �m FBGs have been measured with values of
�6:8 pm �C−1 and �13 pm �C−1 respectively (Morey et
al 1989, Rao et al 1995b). Table 3 gives a summary
of the wavelength–strain and wavelength–temperature
sensitivities for FBGs with different wavelengths (Morey
et al 1989, Xu et al 1994b and Rao et al 1995b).
2:2:3. Pressure. For a pressure change of 1P , the
corresponding wavelength shift 1�BP is given by
1�BP
�B
D 1.n3/
n3
D
�
1
3
@3
@P
C 1
n
@n
@P
�
1P: (11)
In the weakly guided single-mode region, the contribution
to the fractional change in optical propagation delay arising
from a small fractional change in fibre diameter due to
the applied pressure is negligible when compared with the
change in refractive index and physical length. The changes
in physical length and refractive index are given by (Hocker
1979, Morey et al 1992)
1L
L
D − .1− 2�/P
E
(12a)
1n
n
D n
2P
2E
.1− 2�/.2�12 C �11/ (12b)
where E is Young’s modulus of the fibre. As a result
of 1L=L D 13=3 the normalized pitch-pressure and the
index-pressure coefficients are given by
1
3
@3
@P
D − .1− 2�/
E
(13a)
1
n
@n
@P
D n
2
2E
.1− 2�/.2�12 C �11/: (13b)
By substituting equations (13a) and (13b) into (11), we
obtain the wavelength–pressure sensitivity, given by
1�BP D �B
�
− .1− 2�/
E
C n
2
2E
.1− 2�/.2�12 C �11/
�
1P
(14)
For a Ge-doped FBG at 1.55 �m 1�BP =1P was measured
as −3 � 10−3 nm MPa−1 over a pressure range of 70
MPa (Xu et al 1993b). The pressure sensitivity has been
enhanced by a factor of four by mounting the FBG in a
hollow glass bubble to achieve mechanical amplification
(Xu et al 1996).
2:2:4. Dynamic magnetic field. FBGs can also be used
for dynamic magnetic field detection with the Faraday
effect to induce a slight change in the index of the fibre
experienced by left- and right-circularly polarized light in
an FBG (Kersey and Marrone 1994). In the presence
of a longitudinal magnetic field applied to the FBG, the
index is changed for the two circular polarizations and in
consequence two Bragg wavelengths are obtained, as shown
in figure 3, i.e.
�BC D 2nC3 (15a)
�B− D 2n−3 (15b)
where the subscriptsC and− represent the index and Bragg
wavelength for right- and left-circularly polarized light at
the FBG. For the silica fibre, the sensitivity of this effect is
weak as it is determined by the inherent Verdet constant of
the silica which is only �8�10−1 rad T−1 m−1 at �1:3 �m
wavelength. The change in index is given by
nC − n− D VdH�2� (16)
where Vd and � are the Verdet constant and the
working wavelength and H is the applied magnetic field.
Consequently, the resulting wavelength shift is very small
and has been detected with the interferometric interrogation
scheme which can achieve a very high sensitivity (Kersey
and Marrone 1994). Based on this work, dynamic
measurement of large values of current and voltage would
be possible.
2:2:5. Simultaneous strain and temperature measure-
ment. For quasi-static and static strain measurements,
large temperature variations are common in practical ap-
plications. Hence a temperature compensation for the ef-
fect of ambient temperature fluctuation is required (Farahi
et al 1990). A range of techniques have been proposed
to achieve this goal by measuring strain and temperature
simultaneously.
358
In-fibre grating sensors
Figure 3. Splitting of the Bragg resonance due to the
circular birefringence induced by a magnetic field.
2.2.5.1. Reference FBG method. On a single
measurement of the Bragg wavelength shift it is
impossible to separate the effects of changes in strain
and temperature. Therefore a reference is required for
temperature measurement. The most straightforward way
is to use a separated, strain-free FBG as the temperature
sensor to measure the temperature of the strain sensor
directly (Morey et al 1992, Xu et al 1994a). This reference
FBG is located in the same thermal environment as the
strain sensor. The strain error caused by the temperature
variation can be compensated to first order by subtracting
the wavelength shift induced by temperature variation from
the total wavelength shift obtained with the strain sensor.
It has been found that a chirped FBG in a tapered optical
fibre can be temperature independent (Xu et al 1995). The
taper profile is designed such that the FBG is linearly
chirped when tension is applied, creating a strain gradient
along the FBG. By measuring the effective bandwidth
variation rather than the Bragg wavelength change, the
reflected intensity signal is insensitive to temperature. This
special type of FBG sensor is attractive as no temperature
compensation is required, but one problem is that at the
tapered region of the fibre mechanical strength becomes
much weaker and hence the fibre is easy to break.
Furthermore, investigation might be needed to assess the
measurement accuracy as any intensity fluctuation along
the lead fibre would cause error.
2.2.5.2. Dual-wavelength superimposed FBGs method.
This method is based on the use of two sets of wavelength-
shift data obtained from two superimposed FBGs written at
the same location in the fibre (Xu et al 1994b). Assuming
that the wavelength shifts in strain and temperature are
linear, the Bragg wavelength-shift, 1�B , in response to a
strain change, 1", and a temperature change, 1T , is given
by