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Temperature-modulated bioluminescence tomography

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Abstract

It was recently reported that bioluminescent spectra can be significantly affected by temperature, which we recognize as a major opportunity to overcome the inherent illposedness of bioluminescence tomography (BLT). In this paper, we propose temperature-modulated bioluminescence tomography (TBT) to utilize the temperature dependence of bioluminescence for superior BLT performance. Specifically, we employ a focused ultrasound array to heat small volumes of interest (VOI) one at a time, and induce a detectable change in the optical signal on the body surface of a mouse. Based on this type of information, the BLT reconstruction can be stabilized and improved. Our numerical experiments clearly demonstrate the merits of our TBT with either noise-free or noisy datasets. Also, this idea is applicable in 2D bioluminescence imaging and computational optical biopsy (COB). We believe that our approach and technology represents a major step forward in the field of BLT, and has an important and immediate applicability in bioluminescence imaging of small animals in general.

©2006 Optical Society of America

1. Introduction

The function of molecular imaging is to help study biological processes in vivo at the cellular and molecular levels [1, 2, 3, 4, 5]. It may non-invasively differentiate normal from diseased conditions. The imaging of molecular signatures, specific proteins and biological pathways allows early diagnosis and individualized therapies, leading to the so-called molecular medicine. While some classic techniques do reveal information on micro-structures of the tissues, only recently have molecular probes been developed along with associated imaging technologies that are sensitive and specific for detecting molecular targets in animals and humans. A molecular probe has a high affinity for attaching itself to a target molecule and a tagging ability with a marker molecule that can be tracked outside a living body. Among molecular imaging modalities, optical imaging, especially fluorescence and bioluminescence imaging, has attracted remarkable attention for its unique advantages, especially performance and cost-effectiveness.

Among various optical molecular imaging techniques, bioluminescence tomography (BLT) [6, 7, 8] is an emerging and promising bioluminescence imaging modality. In contrast to fluorescent imaging, there is no background auto-fluorescence with bioluminescence imaging. The introduction of BLT relative to planar bioluminescence imaging can be, in a substantial sense, compared to the development of x-ray CT based on radiography. Without BLT, bioluminescence imaging is primarily qualitative. With BLT, quantitative and localized analyses of a bioluminescent source distribution become feasible in a mouse.

Optical molecular imaging of mice is of paramount importance because of the availability of genetically homogeneous inbred strains of mice and the creation of transgenic strains carrying activated and inducible forms of oncogenes or knockouts of tumor suppressive genes. Mice are used in over 90% of mammalian research studies. Mouse models are established for over 90% of human diseases. Currently, results from leading groups all suggest that in favorable cases with strong prior knowledge BLT can produce valuable tomographic information [7, 9, 10, 8, 11, 12, 13, 14, 15, 16, 17, 18, 19]. One category of the favorable cases is that a relatively small source permissible region is known prior to the BLT reconstruction. Nevertheless, it is not always reliable or feasible to define such a permissible region effectively. In brief, it remains extremely challenging to achieve a significantly better and consistently stable BLT performance.

Zhao et al. have recently reported that bioluminescent spectra can be significantly affected by temperature [20]. As it is well known, when the luciferase is combined with the substrate luciferin, oxygen and ATP, biochemical reactions occur to emit bioluminescent photons. Luciferase enzymes from firefly (FLuc), click beetle (CBGr68, CBRed), and Renilla reniformins (hRLuc) have different emission spectra that are temperature dependent. When temperature is increased from 25°C to 39°C, the brightness increases in general. Moreover, FLuc has a 34 nm spectral red shift, as shown in Fig. 1 [20].

 figure: Fig. 1.

Fig. 1. Spectra of FLuc at 25°C, 29°C, 33°C and 37°C (data from [20] with permission).

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The Fluc spectrum may be partitioned into the following three bands: [500,590], [590,625], and [625,750] nm. The first spectral interval covers cyan, green and yellow. The second interval is essentially for orange. The last interval is for red. The rationale for this particular partition is that these intervals contain very similar amounts of bioluminescent energy at the mouse body temperature 37°C. Table 1 lists percentages of energy in each spectral band along with the normalized total energy at different temperatures. While the original data in the temperature range [25°, 39°]C are available [20, 21], the data at 41°C are from a third order polynomial extrapolation with least-square fitting.

Tables Icon

Table 1. Percents of energy in each spectral band along with the normalized total energy at different temperatures (The data from 25°C to 39°C are from [20, 21] with permission). The data at 41°C are from our extrapolation. The total energy is normalized by the total energy at 37°C.

We have recognized the aforementioned temperature dependence of bioluminescence as a major opportunity to overcome the inherent illposedness of bioluminescence tomography (BLT). As shown in Table 1, from 25°C to 41°C the total emitted energy is increased as much as about 80%. While the energy percentages in [590,625] nm and [625,750] nm become gradually larger, that in [500,590] nm is accordingly reduced. More interestingly, when the temperature is elevated from 37°C to 41°C, the total energy in [590–750] nm will be increased by about 17%. In bioluminescence imaging, such a magnitude of a bioluminescent source change can be reliably recorded on the body surface of a mouse. For that purpose, we need to heat a bioluminescent source region in a well-controlled manner. If such a heated target is small, we will actually be able to pinpoint a source location and quantify it assuming a known physical model of the mouse. If the heated volume is not that small, we can at least delimit a much-reduced bioluminescent source permissible region, which will in turn greatly improve the BLT reconstruction quality.

In this paper, we propose to develop the first temperature-modulated bioluminescence tomography (TBT) system [22]. Our fundamental idea is to produce a small hot spot (or a differently shaped volumetric region) in a living mouse, and measure the signal of difference on the body surface of the mouse for BLT. The key components of a TBT system include a heating system such as a focused ultrasound array and a traditional BLT system. It is the temperature-modulated, spectrally and temporally resolved data collected using the TBT system that allows us to convert the ill-posed BLT problem into a better-conditioned or well-posed TBT one, and promises major gains in the BLT reconstruction performance in terms of localization, quantification and robustness. In the second section, we describe the ultrasound heating principles and a design of a focused ultrasound array. In the third section, we formulate the temperature-modulated bioluminescence imaging process and present a TBT algorithm. In the fourth section, we report our numerical simulation results. In the last section, we discuss relevant issues and conclude the paper.

2. Ultrasound heating

2.1. System design

Ultrasound has been widely used for heating in hyperthermia. In non-elastic media such as water and tissue, ultrasound energy of low intensity can be directly converted into heat by inelastic scattering. More dramatic heat production is due to the cavitation [23, 24]. Although diagnostic ultrasound normally operates at the frequency range of 1–20 MHz [25], the penetration depth of high frequency ultrasound waves is very short. Therefore, frequencies of 1–3MHz are commonly used to achieve up to 60 mm penetration depth [26] in tissue. Typically, ultrasound is generated using transducers made of piezoelectric materials. The resonance frequency of an ultrasound transducer depends on its size, shape and thickness, and can be modeled by plate and beam theory [27, 28]. Many ultrasound heating devices are constructed under the name of high intensity focused ultrasound (HIFU) [25, 29, 30, 31, 32, 33, 34, 35, 36, 37], which are made in a disk shape to focus into a small volume. The HIFU systems are mostly designed for large areas (a few centimeters in each dimension) and high temperatures (up to 80°C), see Ref. [38] for a review.

Hyperthermia has a cytotoxic effect on the cells. It causes responses in cell membranes, cytoskeleton, cellular proteins, nucleic acids and cellular immune systems [39]. After exposure to greater than 42°C for sufficiently long time, cells develop thermotolerance as an antagonist of the hyperthermic cell death. Hyperthermia also enhances the cytotoxicity of various antineoplastic agents. It induces alternations of blood flow and changes in microenvironment. An internal temperature above 50°C (122°F) will lead to immediate cell death. In this TBT project, we heat each tissue spot up to 43°C for a relatively short time period.

To improve the heating locality, a cylindrical transducer array was designed by Lu at al. [40]. This array was mounted on a 3D translation table. Numerical simulation of similar systems was reported by Ju at al. [41]. However, these applicators were intended for breast hyperthermia. Their control parameters are unsuitable for TBT of small animals. Only recently, Singh et al. designed a small animal hyperthermia ultrasound system (SAHUS) to study tumour hypoxia [42, 43, 44]. The SAHUS consisted of an acrylic applicator with up to four 5MHz ultrasound transducers, a 10-channel RF generator, a 16-channel thermocouple thermometer, and a PC. The system allows real-time temperature feedback control of power deposition. It can produce hyperthermia within a narrow temperature range (regulation error: 0.02±0.01°C) around 41.5°C. Although this system uses non-focused ultrasound transducers, it can heat small tumors of 8 mm in diameter with the aid of interstitial thermocouples. Clearly, it is desirable for TBT to produce a smaller heated volume without interstitial thermocouples.

 figure: Fig. 2.

Fig. 2. The cylindrical ultrasound transducer array system. The surface of each transducer is a part of a large sphere of radius R, centered at the origin of the coordinate system.

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As shown in Fig. 2, we propose to use a cylindrical focused ultrasound array system to demonstrate the feasibility of TBT. The ultrasound applicator is a multi-transducer array mounted on a cylindrical supporter of 10 cm diameter. The applicator may be mechanically moved with respect to the mouse so as to scan a sufficiently large volume of interest with a precision of 0.2 mm in each dimension. The spherical focusing transducers are driven by multichannel RF generators containing function generators and power amplifiers under PC control.

2.2. Pressure field expression

The ultrasound absorption power density can be estimated using an empirical formulas based on the exponential decay law of ultrasound intensity in tissue [45]. The specific absorption rate can be computed from the ultrasound pressure distribution. The ultrasound wave propagation in lossy media is usually associated with dispersion and acoustic attenuation, typically exhibiting a frequency dependency [46]. A more sophisticated treatment involves a time-domain attenuation model and multiple relaxation channels [47, 48, 49, 50, 51, 52, 53, 54, 55].

Ultrasound motion is governed by the wave equation, which gives rise to the Helmholtz equation in the frequency domain via the time harmonic approximation [56]. The full wave modeling of therapeutic ultrasound propagation in fluids was provided by Ginter et al. [57]. Alternatively, the equation for the sound pressure can be derived from the Navier-Stokes type of equations of gas dynamics. Using the conservation laws of mass and momentum, Liebler et al. [58] derived hyperbolic equations for the ultrasound pressure field. McGough et al. [59, 60] developed an efficient grid sectoring method for calculation of the near-field pressure.

In our system of Nt spherical focusing transducers targeting the center of the cylindrical ring, the pressure field at a given position x can be estimated from the Rayleigh-Sommerfeld radiation integral equation [61, 62]

p(x)=iρcλSue(α+ik)xxxxdS,

where S′ denotes the total surface area of the transducers, ρ the density of the medium, c the phase velocity of the sound wave, u the velocity amplitude, λ the wavelength, k the wavenum-ber, α the attenuation coefficient, and x′ ∈ S′. The surface of each spherical focusing transducer can be partitioned into N rectangular elements. For a sufficiently fine partition, the formula by Ocheltree and Frizzell [61] can be modified to calculate the pressure field at x

p(x)=m=1Nt(iρchxhyλ)n=1NunLne(α+ik)Lnsinckxnhx2Lnsinckynhy2Ln

where x′n = (xn,yn,zn) gives the coordinates of x in the local coordinate system associated with the nth element (the origin at the center of the element, the z-axis passing through the focusing center of the transducer), Ln is the distance between x and the center of the element, hx and hy are the lengths of the element along the x′n - and y′n -axes respectively, un=2WρcA is the velocity amplitude with radiation power W of a transducer, and A=2πR2(11d24R2) the surface area of the transducer, where d is the diameter of the transducer, and R the radius of the cylinder.

2.3. Bioheat transfer model

To reduce reflection, both the ultrasound applicator and the corresponding part of the mouse body surface are immersed in water during the heating process. Then, we can assume that the density and the speed of ultrasound in two layers are sufficiently close so that reflection and refraction at the water-tissue interface are negligible [40, 63]. Furthermore, the ultrasound power deposition can be regarded as stationary.

The ultrasound thermal transport process in phantom and in vivo is modeled using Pennes’ bioheat transfer equation [64, 40, 65]

ρctTt=κ2Tcbω(TTa)+Q,

where ρ is the tissue density, T the temperature field, Ta the normal body temperature of the mouse (also the water temperature), κ the thermal conductivity of the tissue, ct and cb are the specific heat of tissue and blood, respectively, ω is the blood perfusion rate, Q the absorption power density given as Q = ρq, and q is the specific absorption rate. We have [65, 41]

q=αp2ρc,

where α is the ultrasound absorption coefficient of tissue, c the speed of sound, and p the ultrasound pressure field. At each point, the specific absorption rate can be calculated as the sum of the contributions from all of the transducers. As heating time is relatively long and the heating power is relatively low, the temperature fluctuation can be neglected. Thus, a steady state bioheat transport equation is obtained as follows:

κ2Tcbω(TTa)+Q=0.

3. Image reconstruction

3.1. BLT formulation

Since TBT is an extension of BLT, let us first give an overview of the BLT formulation in the single and multispectral cases, using the notation in [8]. Bioluminescent photon scattering dominates over absorption in the biological tissue. Hence, this photon transport process can be modeled by the following steady-state diffusion equation [66, 8]:

{(D(x)Φ(x))+μa(x)Φ(x)=S(x)(xΩ)D(x)=(3(μa(x)+(1g)μs(x)))1Φ(x)+2AxnnD(x)(v(x)Φ(x))=0(xΩ)

where Ω denotes the region of interest, Φ(x) the photon fluence [Watts/mm2] at location x, S(x) the bioluminescent source density [Watts/mm3], μa (x) the absorption coefficient [mm-1], μs (x) the scattering coefficient [mm-1], g the anisotropy parameter, ∂Ω the boundary of Ω, v the unit outer normal on ∂Ω,A(x;n,n′) a function depending on the refractive indices n for Ω and n′ for the surrounding medium. Since both the ultrasound applicator and the corresponding part of the mouse body surface are immersed in water in the heating process, the surrounding medium is water with nn′ = 1.33. In this case A (x;n,n′) ≈ 1. In our study, we assume that the bioluminescence imaging experiment is performed in a totally dark environment. The outgoing photon density on ∂Ω is:

Q(x)=D(x)(vΦ(x))=Φ(x)(2Axnn)(xΩ)

Then, the BLT problem is to determine a source S given measurement data Q based on Eq. (6).

Using the finite-element method to solve the BLT problem, we have [8]:

[M]{Φ}=[F]{S}.

Furthermore, we can write Eq. (8) as

[M1,1M1,2M1,2TM2,2]{Φ˜Φ*}=[F1,1F1,2F2,1F2,2]{SpS*},

where Φ˜ represents the measurable photon density values of the finite element nodes on the boundary ∂Ω, and Φ* the photon density values of the internal nodes, while the source vector S is divided into Sp in a permissible region Ωs and S * = 0 in the forbidden region. The permissible region is where a bioluminescent light source may exist, while the forbidden region is where no bioluminescent light source could exist. Now the equation can be reduced to [8]

Φ˜=BSp,

where B = (M 1,1 -M 1,2 M2,21-M1,2T)-1(F 1,1 - M 1,2-M2,21-F 2,1).

In a BLT experiment, the output photon flux Q(x) from a mouse is captured with a CCD camera. By Eq. (7), the photon density on the mouse body surface can be obtained from Q(x). With the measurement of Φ˜ denoted as Φm, our problem is to recover the source Sp from Φm based on Eq. (10). Since the measured data are necessarily corrupted by noise, it is not optimal to invert Eq. (10) strictly. We minimize the following objective function to perform a BLT reconstruction:

O(Sp)=(Φ˜Φm)TW(Φ˜Φm)+εη(Sp),

where W denotes weighting matrix, η a stabilizing function, ε a regularization parameter [8]. In our study, we set η(X) = XTX. Although the regularizaion method is widely used to overcome the ill-posedness of an inverse problem, there is not a well-accepted governing theory on the optimal selection of the stabilizing function and its regularization parameter. If the problem is more strongly regularized, the solution will be more stable but the error will be larger. In general, the regularization method must be fine-tuned in the simulation and experiments.

Now, we are ready to formulate multi-spectral BLT (MBLT) as an extension of the above single-spectral formulation. First, let us assume no knowledge on the spectral profile of an underlying bioluminescent source, such as in the case of mixed bioluminescent probes with unknown concentrations. At each wavelength of interest λi , we have

Φ˜λi=BλiSλip.

The corresponding objective function is

OM(Sp)=i=1n((Φ˜λiΦλim)TWλi(Φ˜λiΦλim)+ελiηλi(Sλip)),

where n is the number of spectral bands, W λi a weighting matrix for spectrum λi . Then, the MBLT problem is just to find minimizers for OM(Sp ). In a more general scenario, there are several bioluminescent probes working together, these probes may have different temperature-dependent spectra. To recover the concentrations of these probes, we assume that the underlying source contain k bioluminescent probes Pj with corresponding spectral weights wPiλi , j = 1,…,k. By solving the following linear system, Xj (the power for Pj ) can be recovered.

[wλ1P1wλ1PkwλnP1wλnPk][X1Xk]=[(Sλ1p)T(Sλnp)T]

Clearly, nk is needed for a unique solution to the linear system. Note that in the case of only one bioluminescent probe in a mouse, Eq. (12) can be enhanced as [13]

Φ˜λi=wλiBλiSp,and
OM(Sp)=i=1n((Φ˜λiΦλim)TWλi(Φ˜λiΦλim)+ελiηλi(Sp)),

where n is the number of spectral bands, W λi a weighting matrix for spectrum λ i.

3.2. TBT algorithm

In the TBT process, we first record bioluminescent data on the body surface of a mouse at the body temperature, and may perform a regular BLT reconstruction. Based on all the information we collect, we can determine which regions should be heated for improvement of the BLT reconstruction. For example, we may evaluate all the elements in the permissible region via a cluster analysis, which is a well-established methodology in pattern recognition to merge finite elements of bioluminescent sources into localized groups. Then, we may use minimal spheres to cover identified clusters, and heat each of such spheres to collect bioluminescent data again. If there is a significant difference between the data before and after heating, a TBT reconstruction will be performed from the difference signal for the heated volume. If any heated volume does not produce a significant change in the bioluminescent signal, the previous BLT reconstruction in that region is considered invalid, and we need to select a different permissible region. Generally speaking, any body region R in a mouse can be heated to determine if there exists any bioluminescent source, and if so we can perform a TBT reconstruction based on the difference data measured on the mouse body surface before and after heating. Assuming that the temperature-dependent spectrum of the bioluminescent probe is known, we have the following two major TBT cases that involve (i) spectrally mixed and (ii) multi-spectral datasets, respectively.

In the case of a spectrally mixed dataset, at the reference temperature (the body temperature), we have

Φ˜=i=1nwλiBλiSIp+i=1nwλiBλiSOp,

where SIp and SOp are the source vectors inside and outside the heated region, respectively. After heating, we have

Φ˜H=ti=1nwλiBλiSIp+i=1nwλiBλiSOp,

where t is the normalized total energy at the elevated temperature, as shown in Table 1, wλi denotes the spectral weight at λi at the elevated temperature, and w λi and wλi are available in Table 1. Now, let us compute the signal difference again,

Φ˜D=Φ˜HΦ˜=i=1n(twλiwλi)BλiSIp.

Therefore, we have the following objective function for TBT:

O(SIp)=(Φ̃DΦDm)TW(Φ˜DΦDm)+εη(SIp),

where W is a weighting matrix.

In the case of a multi-spectral dataset, for each spectral band we have

Φ˜λi=wλiBλiSIp+wλiBλiSOp.

After heating, we have

Φ˜H,λi=twλiBλiSIp+wλiBλiSOp.

Then, the difference signal and the objective function become

Φ˜D,λi=Φ˜H,λiΦ̃λi=(twλiwλi)BλiSIp,and
OM(SIp)=i=1n((Φ˜D,λiΦD,λim)TWλi(Φ˜D,λiΦD,λim)+ελiηλi(SIp)),

where W λi is a weighting matrix for spectrum λi .

Assuming that there are a number of temperature-dependent spectra from multiple kinds of bioluminescent probes, we generally do not know the concentrations of these probes at any particular location. In this case, we can perform a TBT reconstruction for each spectral band. After the bioluminescent power in each band is obtained, we can solve a linear equation system similar to Eq. (14) for 3D reconstruction of the concentrations of these probes.

4. Simulation results

4.1. Ultrasound heating simulation

The simulation was carried out on a workstation with a FORTRAN code. The standard second order finite difference scheme was used for discretizing the bioheat equation. A resolution of 0.1 mm/MHz was used to ensure the accuracy. In our simulation, we set the average speed of sound c = 1540 m/s, the specific heat of tissue ct = 4186 J/kg °C and the ultrasound absorption coefficient α= 8.6 fm1.5 Np/m [67, 68, 41, 65].

 figure: Fig. 3.

Fig. 3. Plots of the Q distribution on the plane z = 0 for ω= 1.5 kg m-3 s-1, R = 5 cm and d = 0.635 cm. (a) f = 1, Nt = 17; (b) f = 2, Nt = 29; (c) f = 3, Nt = 41.

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 figure: Fig. 4.

Fig. 4. Plots of the Q distribution on the plane z = 0 with different Nt values for f = 2 MHz, w= 1.5 kg m-3 s-1, R = 5 cm, and d = 1.27 cm. (a) Nt = 11, (b) Nt = 19, and (c) Nt = 29.

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4.1.1. Absorption power density distributions

We first examined the effect of frequency as it primarily determines the focus radius in the heating process. We selected three frequencies, f = 1,2 and 3 MHz. In all the cases, we made ω= 1.5kgm-3s-1,R = 5cm,d = 0.635cm. For f = 1,2, and 3 MHz, the number of transducers Nt was set to 17, 29 and 41, respectively. As shown in Fig. 3, the contour plots tightly surround the focus center, showing that the focus radius was 3, 1.5 and 1 mm for f = 1, 2, and 3 MHz, respectively. That is, with f = 2 or 3 we can obtain the desired absorption power density distribution.

Then, we fixed f = 2 MHz without loss of generality and examined the effects of other parameters. The transducer array was meant to achieve constructive-interference at the focus center and destructive-interference elsewhere. Imperfect interference led to undesired sidelobes. Since the geometry was fixed, the second most important parameter is the number of transducers Nt . Figure 4 depicts the impact of Nt on the plane z = 0. Clearly, when Nt = 11 only a small region that was very close to the focus center had a desired destructive-interference, while undesired sidelobes were scattered widely. When Nt = 19 the heating locality was much improved. When Nt = 29 an ideal absorption power density distribution was obtained. Actually, for a given frequency there is a critical number of transducers Nc to achieve a desired absorption power density distribution. As the frequency becomes higher, Nc becomes larger. For f = 1,2 and 3, Nc = 15,29 and 39, respectively. On the other hand, the maximum number of transducers is limited by Interestingly, the increment in the number of transducers did not affect the size of the central peak cross section. The diameter of the central peak cross section is about four times of the wavelength. That is, although the sound wave does not propagate in specific direction, it can be effectively focused via appropriate interference.

 figure: Fig. 5.

Fig. 5. Plots of the Q distribution on the plane z = 0 with different R values for f = 2 MHz, ω= 1.5 kg m-3 s-1, d = 0.635 cm, and Nt = 29. (a) R = 4 cm, (b) R = 5 cm, and (c) R = 6 cm.

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 figure: Fig. 6.

Fig. 6. Plots of the Q distribution on the plane z = 0 with different d values for f = 2MHz, ω= 1.5 kg m-3 s-1, R = 6 cm and Nt = 29. (a) d = 0.635 cm and (b) d = 1.27 cm.

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Figures 5 and 6 show the effects of the focus length R and the diameter d. These plots were visually similar. The only very small changes were observed in the maximum intensities with respect to different R and d values.

4.1.2. Temperature distributions

Having examined the impact of various dimensional parameters on the absorption power density distribution, we investigated how the temperature distribution was controlled by the transducer power and the blood perfusion rate. It was found that W did not change the shape of Q but affected its magnitude. Consequently, the maximum temperature T max was a function W. Moreover, W had only a scaling effect on Q, and thus its effect on the temperature increment (T max - Ta ) is linear (Ta = 37°C). In other words, with the other parameters fixed, the temperature increment is increased twice if the power W doubled, as shown in Fig. 7.

Finally, we investigated the impact of the blood perfusion rate ω. Figure 8 shows representative results for ω= 0.5kgm-3s-1 and ω= 3.5kgm-3s-1. It was seen that the temperature peak became sharper for a larger perfusion rate. On the other hand, ω only rescaled the steady state temperature but did not change its profile shape. In particular, the smaller ω was, the weaker its cooling effect, and the less the power W would be needed, as illustrated in Fig. 8.

In Tables 2, 3 and 4, we summarize the recommended control parameters for f = 1,2,3MHz, respectively. In these cases, Ta = 37°C, the maximum temperature was set to 43°C, and the number of transducers was minimized. Also, included in the tables are different perfusion rates, focus lengths and transducer diameters.

 figure: Fig. 7.

Fig. 7. Plots of the T distribution on the plane z = 0 with different W values for f = 2 MHz, ω= 1.5 kg m-3 s-1, R = 4 cm and d = 0.635 cm. (a) W = 0.008 w and (b) W = 0.016 w.

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 figure: Fig. 8.

Fig. 8. Plots of the T distribution on the plane z = 0 with different ω values for f = 2 MHz, R = 4 cm and d = 0.635 cm. (a) ω= 0.5 kg m-3 s-1, W = 0.018w and (b) ω = 3.5 kg m-3 s-1, W = 0.025 w.

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Tables Icon

Table 2. Recommended control parameters for f = 1 MHz.

While the cylindrical array design allows an excellent absorption power density distribution on the xy plane, we now determine how the absorption power density is distributed along the z-axis. Figure 9 shows the absorption power density at the x = 0 cross section. The plot at the y = 0 cross section is identical. Although the absorption power density distribution is symmetric on the xy plane, there is an undesired power absorption off the focus center along the z-direction.

Tables Icon

Table 3. Recommended control parameters for f = 2 MHz.

Tables Icon

Table 4. Recommended control parameters for f = 3 MHz.

 figure: Fig. 9.

Fig. 9. Longitudinal extent of the Q distribution over the plane x = 0. (a) Surface plot and (b) a contour plot for f = 2 MHz, ω = 1.5 kg m-3 s-1, R = 4 cm, d = 0.635 cm and Nt = 29.

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In Fig. 10, temperature distributions are further analyzed along the z-axis. These quantities of interest are plotted over the yz cross section. It is shown that the size of high temperature region (T > 40°C) is less than 1 cm. Technically, it is feasible to reduce the longitudinal extent of the heated volume using a few more focusing arrays.

 figure: Fig. 10.

Fig. 10. Longitudinal extent of the T distribution over the plane x = 0. (a) Surface plot and (b) a contour plot for f = 2 MHz, ω = 1.5 kg m-3 s-1, R = 4 cm, d = 0.635 cm, and Nt = 29.

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 figure: Fig. 11.

Fig. 11. Finite element model of the mouse chest phantom.

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4.2. TBT reconstruction

We tested the above-proposed TBT algorithm in the numerical simulation using a mouse chest phantom. This anatomically realistic phantom was digitally built from an MRI mouse atlas (http://www.mrpath.com/visiblemouse.html). Specifically, based on a segmented MRI image volume we obtained a finite-element model of the mouse chest as shown in Fig. 11. This phantom consisted of lungs, a heart, a liver, and muscle. The appropriate absorption μa and reduced scattering μ′s coefficients were assigned to these anatomical structures as shown in Table 5, which were extracted from the literature [16, 69, 70, 71].

As mentioned before, among the four kinds of luciferase enzymes: hRLu, CBGr68, CBRed, and Fluc, only FLuc has not only an increment in the emission power but also a red-shift in the spectrum with temperature elevation. As a result, in this feasibility study we only used FLuc as the bioluminescent probe. As shown in Table 1, we have the original spectral data from 25°C to 39°C, and the extrapolated data at 41°C.

In our numerical simulation, we put respectively single and double bioluminescent sources in the mouse phantom, and performed TBT reconstructions from either spectrally mixed or multi-spectral datasets. In our tests, we partitioned the spectra over the interval [500,750] nm into the following three portions: (a) [500,590] nm, (b) [590,625] nm, and (c) [625,750] nm. We further assumed that in each portion the optical parameters would remain the same with temperature change. Since the normal temperature is 37°C, we set the elevated temperature to 41°C. From Table 1, w a,37° = 0.2844, w b,37° = 0.3264, w c,37° = 0.3892, w a,41° = 0.2340, w b,41° = 0.3335, w c,41° = 0.4325, and t = 1.0921. In all the cases, each source had a power of 10-picowatt (about 3 × 107 photons per second) and limited within an finite-element. The camera was on for 600 seconds. The measurement data on the side surface of the phantom were generated according to the finite-element-based diffusion model Eq. (8). Because the number of emitted photons follows a Poisson distribution, we added Poisson noise to these data [72]. Then, we added 5% and 10% Gaussian noise to the Poisson data respectively to reflect the non-Poisson noise/biases in the measurement process. Figures 12 and 13 show the simulated optical data and the difference signals with one and two bioluminescent sources in the phantom, respectively.

Tables Icon

Table 5. Optical parameters of various anatomical structures in different spectral bands.

 figure: Fig. 12.

Fig. 12. Optical data on the side surface of the finite-element phantom containing one bioluminescent source. (a) Original optical data, and (b) the corresponding difference data.

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Based on the geometrical model of the mouse, its optical parameters keyed to each anatomical region, and two surface optical measurement datasets before and after heating, the TBT algorithm can be applied to produce reliable results on the location and power of the bioluminescent source. Table 6 summarizes the representative TBT results. In each case, we reconstructed the source distribution 10 times. In all the tests, the source locations were randomly chosen while the same geometrical model and the same optical properties were used. It can be seen in Table 6 that the TBT algorithm worked very well.

 figure: Fig. 13.

Fig. 13. Optical data on the side surface of the finite-element phantom containing two bioluminescent sources. (a) Original optical data, (b) the corresponding difference data, (c) an oblique section showing the source locations (red), reconstructed source localtion (blue) and a heated region (green), and (d) an oblique section showing the photon density distribution. Sources 1 and 2 were inside and outside the heated volume, respectively.

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5. Discussions and conclusion

The simulation results on ultrasound heating have confirmed the feasibility of our focused ultrasound array design. We have analyzed the impact of a wide range of physical parameters on the absorption power density and temperature distributions, involving ultrasound frequency, transducer diameter, focal length, output power, number of transducers, spatial arrangement, blood perfusion rate, and so on. Our results have indicated that the heating locality is mainly controlled by the ultrasound frequency and spatial arrangement of the transducers. Although the use of a higher frequency leads to a smaller heated volume, it requires a larger number of transducers to suppress sidelobes. Our results have provided the guidelines for minimization of the heating locality and the number of transducers for a given frequency. Such a highly localized heating capability is instrumental for our proposed TBT.

While a cylindrical transducer array has been analyzed to produce a small hot spot in a small animal, other configurations for ultrasound heating and other kinds of heating means are possible as well and may be advantageous in some sense. For example, a spherical focusing array can be used to improve the heating locality. It is also possible to use an annular phased ultrasound array system to heat a nude mouse with coupling gel (without the use of water immersion). Such a system can achieve the whole-body access, although its locality may not be as good as the cylindrical design. On the other hand, we may design ultrasound array systems for heating a transverse slice or a linear path in a living animal. For example, a low frequency ultrasound beam can heat a cross-section of thickness four times of the ultrasound wavelength. To heat a relatively large volume, radio frequency (RF) below 20 MHz and microwave (MW) above 100 MHz are feasible options too. To achieve better resolution, high frequency MW should be used. However, the penetration length of RF and MW decreases with increment in frequency. For both RF current and MW radiation, absorbed power density decreases exponentially with the depth in tissue. Consequently, it is technically impossible to achieve both fine locality and deep penetration using either RF or MW applicators. Also, ultrasound, RF and/or MW may be combined for synergy.

Tables Icon

Table 6. Simulated TBT results in the cases of single and double sources from spectrally mixed and multi-spectral datasets in terms of source localization and power estimation errors.

It is recognized that our heating-related computation can be improved by compensating for the anatomical heterogeneity. Indeed, sound speed varies about 3 percents inside the mouse body. Other spatially variant properties are blood profusion rate, thermal conductivity, specific heat, ultrasound absorption coefficient, reflection and scattering of ultrasound waves from acoustic impedance boundaries such as at the surfaces of bone and lungs. Since BLT is typically solved using a multi-modality approach, an independent tomographic volume of an individual mouse is assumed to be already available. Hence, a more sophisticated ultrasound focusing scheme can be developed to take into account the heterogeneous anatomy of the mouse under study, which is however beyond the scope of this paper. Nevertheless, with more accurate modeling and proper calibration, the inhomogeneous effect can be effectively incorporated, leading to better performance of the TBT system. Additionally, both ultrasound heating and ultrasound imaging may be performed using a single ultrasound device. Such an integrated system would allow more precise control of the heating process and monitoring of the temperature change, which can be improved by analysis of resultant optical measurement on the mouse body surface.

Furthermore, strictly speaking all of the physical parameters are temperature-dependent, which include mass density, sound speed, profusion rate, thermal conductivity, specific heat, and ultrasound absorption coefficient. It is possible to include thermal coupling effects in our computation. Nevertheless, these effects are very small in our case since the temperature increment is only a few degrees. Hence, we have not incorporated them in this feasibility study.

By heating a relatively small region and extracting the difference signal, the permissible region for bioluminescent source reconstruction is dramatically reduced. This helps tremendously regularize an ill-posed BLT problem into a better-conditioned or well-posed TBT framework. The original BLT algorithm highly depends on the specification of the permissible region. If such a region is incorrectly outlined or made too large, the BLT reconstruction will not be accurate and stable. Fortunately, this challenge has now been effectively addressed using the TBT approach. With ultrasound heating and difference signal detection, it becomes practical to be certain if the bioluminescent probe exists in any specified small volume. Hence, the reconstruction performance of TBT can be made significantly superior to that of traditional BLT. In all the 80 simulation runs we have performed so far, it has been found that the source localization and power estimation can be satisfactorily done with on average < 1mm and < 25% errors, respectively.

After a TBT reconstruction, the bioluminescent source distribution can be further refined based on the original bioluminescent data measured on the mouse body surface at the normal temperature (37°C). Since the TBT reconstruction may contain substantial errors due to data noise, model mismatches, system biases and so on, the computed bioluminescent data on the mouse body surface based on the TBT reconstruction may not explain the original data very well. This actually presents us a major opportunity to improve the TBT reconstruction according to the original data. For example, if we assume that the spatial support and relative variation of the bioluminescent source distribution reconstructed in the TBT are quite reliable, then we can scale the bioluminescent source distribution obtained in the TBT reconstruction so that the computed surface bioluminescent measurement fits the original data optimally. More sophisticatedly, we can statistically characterize all the sources of the imperfection in the TBT process, and perform the correction based on more quantitative constraints and more specific models.

While in this paper we have focused on 3D TBT reconstruction, it is emphasized that this idea is applicable in 2D bioluminescence imaging [3, 4, 5] and computational optical biopsy (COB) [73, 74]. The temperature-dependent spectra of the bioluminescence may also be utilized in biomedical imaging based on the bioluminescence resonance energy transfer (BRET) phenomena. We believe that our methodology and technology represent a major step forward in the field of BLT, and have a broad, important and immediate applicability in bioluminescence imaging of small animals.

In conclusion, for the first time we have proposed temperature-modulated bioluminescence tomography (TBT) and demonstrated its feasibility. Specifically, we have designed an exemplary focused ultrasound array to heat one small volume of interest (VOI) each time in a living mouse, and induce a detectable change in the optical signal on the mouse body surface. Based on this type of information, the TBT reconstruction has been simulated with excellent results. Currently, we are constructing the first TBT prototype including a focused ultrasound array. Phantom experiments and mouse studies using the TBT system will be reported in the future.

Acknowledgments

The authors thank Dr. Timothy Doyle (Stanford University) for discussion with Dr. Ge Wang on the temperature-dependence of the bioluminescent spectra and permission for use of their original data in [20, 21], as well as Drs. Ming Jiang (Peking University), Yi Li and Michael Henry (University of Iowa) for constructive comments. This work has been partially supported by NIH/NIBIB grant EB001685.

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Figures (13)

Fig. 1.
Fig. 1. Spectra of FLuc at 25°C, 29°C, 33°C and 37°C (data from [20] with permission).
Fig. 2.
Fig. 2. The cylindrical ultrasound transducer array system. The surface of each transducer is a part of a large sphere of radius R, centered at the origin of the coordinate system.
Fig. 3.
Fig. 3. Plots of the Q distribution on the plane z = 0 for ω= 1.5 kg m-3 s-1, R = 5 cm and d = 0.635 cm. (a) f = 1, Nt = 17; (b) f = 2, Nt = 29; (c) f = 3, Nt = 41.
Fig. 4.
Fig. 4. Plots of the Q distribution on the plane z = 0 with different Nt values for f = 2 MHz, w= 1.5 kg m-3 s-1, R = 5 cm, and d = 1.27 cm. (a) Nt = 11, (b) Nt = 19, and (c) Nt = 29.
Fig. 5.
Fig. 5. Plots of the Q distribution on the plane z = 0 with different R values for f = 2 MHz, ω= 1.5 kg m-3 s-1, d = 0.635 cm, and Nt = 29. (a) R = 4 cm, (b) R = 5 cm, and (c) R = 6 cm.
Fig. 6.
Fig. 6. Plots of the Q distribution on the plane z = 0 with different d values for f = 2MHz, ω= 1.5 kg m-3 s-1, R = 6 cm and Nt = 29. (a) d = 0.635 cm and (b) d = 1.27 cm.
Fig. 7.
Fig. 7. Plots of the T distribution on the plane z = 0 with different W values for f = 2 MHz, ω= 1.5 kg m-3 s-1, R = 4 cm and d = 0.635 cm. (a) W = 0.008 w and (b) W = 0.016 w.
Fig. 8.
Fig. 8. Plots of the T distribution on the plane z = 0 with different ω values for f = 2 MHz, R = 4 cm and d = 0.635 cm. (a) ω= 0.5 kg m-3 s-1, W = 0.018w and (b) ω = 3.5 kg m-3 s-1, W = 0.025 w.
Fig. 9.
Fig. 9. Longitudinal extent of the Q distribution over the plane x = 0. (a) Surface plot and (b) a contour plot for f = 2 MHz, ω = 1.5 kg m-3 s-1, R = 4 cm, d = 0.635 cm and Nt = 29.
Fig. 10.
Fig. 10. Longitudinal extent of the T distribution over the plane x = 0. (a) Surface plot and (b) a contour plot for f = 2 MHz, ω = 1.5 kg m-3 s-1, R = 4 cm, d = 0.635 cm, and Nt = 29.
Fig. 11.
Fig. 11. Finite element model of the mouse chest phantom.
Fig. 12.
Fig. 12. Optical data on the side surface of the finite-element phantom containing one bioluminescent source. (a) Original optical data, and (b) the corresponding difference data.
Fig. 13.
Fig. 13. Optical data on the side surface of the finite-element phantom containing two bioluminescent sources. (a) Original optical data, (b) the corresponding difference data, (c) an oblique section showing the source locations (red), reconstructed source localtion (blue) and a heated region (green), and (d) an oblique section showing the photon density distribution. Sources 1 and 2 were inside and outside the heated volume, respectively.

Tables (6)

Tables Icon

Table 1. Percents of energy in each spectral band along with the normalized total energy at different temperatures (The data from 25°C to 39°C are from [20, 21] with permission). The data at 41°C are from our extrapolation. The total energy is normalized by the total energy at 37°C.

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Table 2. Recommended control parameters for f = 1 MHz.

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Table 3. Recommended control parameters for f = 2 MHz.

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Table 4. Recommended control parameters for f = 3 MHz.

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Table 5. Optical parameters of various anatomical structures in different spectral bands.

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Table 6. Simulated TBT results in the cases of single and double sources from spectrally mixed and multi-spectral datasets in terms of source localization and power estimation errors.

Equations (24)

Equations on this page are rendered with MathJax. Learn more.

p ( x ) = iρc λ S u e ( α + ik ) x x x x dS ,
p ( x ) = m = 1 N t ( iρc h x h y λ ) n = 1 N u n L n e ( α + ik ) L n sin c k x n h x 2 L n sin c k y n h y 2 L n
ρ c t T t = κ 2 T c b ω ( T T a ) + Q ,
q = α p 2 ρc ,
κ 2 T c b ω ( T T a ) + Q = 0 .
{ ( D ( x ) Φ ( x ) ) + μ a ( x ) Φ ( x ) = S ( x ) ( x Ω ) D ( x ) = ( 3 ( μ a ( x ) + ( 1 g ) μ s ( x ) ) ) 1 Φ ( x ) + 2 A x n n D ( x ) ( v ( x ) Φ ( x ) ) = 0 ( x Ω )
Q ( x ) = D ( x ) ( v Φ ( x ) ) = Φ ( x ) ( 2 A x n n ) ( x Ω )
[ M ] { Φ } = [ F ] { S } .
[ M 1,1 M 1,2 M 1,2 T M 2,2 ] { Φ ˜ Φ * } = [ F 1,1 F 1,2 F 2,1 F 2,2 ] { S p S * } ,
Φ ˜ = B S p ,
O ( S p ) = ( Φ ˜ Φ m ) T W ( Φ ˜ Φ m ) + εη ( S p ) ,
Φ ˜ λ i = B λ i S λ i p .
O M ( S p ) = i = 1 n ( ( Φ ˜ λ i Φ λ i m ) T W λ i ( Φ ˜ λ i Φ λ i m ) + ε λ i η λ i ( S λ i p ) ) ,
[ w λ 1 P 1 w λ 1 P k w λ n P 1 w λ n P k ] [ X 1 X k ] = [ ( S λ 1 p ) T ( S λ n p ) T ]
Φ ˜ λ i = w λ i B λ i S p , and
O M ( S p ) = i = 1 n ( ( Φ ˜ λ i Φ λ i m ) T W λ i ( Φ ˜ λ i Φ λ i m ) + ε λ i η λ i ( S p ) ) ,
Φ ˜ = i = 1 n w λ i B λ i S I p + i = 1 n w λ i B λ i S O p ,
Φ ˜ H = t i = 1 n w λ i B λ i S I p + i = 1 n w λ i B λ i S O p ,
Φ ˜ D = Φ ˜ H Φ ˜ = i = 1 n ( t w λ i w λ i ) B λ i S I p .
O ( S I p ) = ( Φ ̃ D Φ D m ) T W ( Φ ˜ D Φ D m ) + εη ( S I p ) ,
Φ ˜ λ i = w λ i B λ i S I p + w λ i B λ i S O p .
Φ ˜ H , λ i = tw λ i B λ i S I p + w λ i B λ i S O p .
Φ ˜ D , λ i = Φ ˜ H , λ i Φ ̃ λ i = ( t w λ i w λ i ) B λ i S I p , and
O M ( S I p ) = i = 1 n ( ( Φ ˜ D , λ i Φ D , λ i m ) T W λ i ( Φ ˜ D , λ i Φ D , λ i m ) + ε λ i η λ i ( S I p ) ) ,
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