In this section we use the parameterizations of Eqs. (14a)–14d)) to obtain the best reconstruction of F(X) based on observational data. In particular, we make use of the Pantheon data set [28] consisting of 1049 SNIa data points. The SNIa data enable us to constrain the luminosity distance \(d_L(z)=(1+z)r(z)\), where r(z) is the comoving distance. We fit the SNIa with the cosmological model by minimizing the \(\chi ^2\) value defined by
$$\begin{aligned} \chi _\mathrm{SNIa}^2 = \triangle \mathbf {\mu }^{T} \cdot \mathbf C ^{-1} \cdot \triangle \mathbf {\mu }, \end{aligned}$$
(20)
where \(\triangle \mathbf {\mu } = \mathbf {\mu } - \mathbf {\mu }_{m} \) and \(\mathbf {\mu }_{m}\) is a vector containing the distance modulus of the model for each redshift,
$$\begin{aligned} \mu _m(z) \equiv 5\log _{10}[d_L(z)/{\texttt {Mpc}}]. \end{aligned}$$
(21)
\(\mathbf C \) is the uncertainty matrix defined by \(\mathbf C = \mathbf D + \mathbf C _\mathrm{sys}\), with \(\mathbf D \) the statistical (diagonal) matrix and \(\mathbf C _\mathrm{sys}\) the systematic covariance matrix.
Actually, there is no need to use (11) and (12) to obtain X(a) and F(a) for a given \(\omega (a)\). In fact, from (4) we know that
$$\begin{aligned} F(a) = \omega (a) \rho (a), \end{aligned}$$
(22)
and from (6) we know that
$$\begin{aligned} 4\kappa X(a) = a^{6}(1+\omega (a))^2\rho (a)^2. \end{aligned}$$
(23)
So, all we need is the expression for \(\rho (a)\). From the mass conservation equation we can write
$$\begin{aligned} \rho (z) = \rho _0 (1+z)^3 \exp \left( 3 \int _0^{z} \frac{\omega (x)}{1+x}\mathrm{d}x \right) , \end{aligned}$$
(24)
where we have introduced the redshift z defined through the relation \(a=(1+z)^{-1}\).
Model A
Let us start with a first case, the one we called Model A, which is defined through its EoS parameter given by \(w(z)=w_0 + w_a z\). Using Eq. (24) we obtain
$$\begin{aligned} \rho (z) = \rho _0 (1+z)^{3(1+w_0-w_a)} e^{3 w_a z}, \end{aligned}$$
(25)
and from Eq. (22) we get
$$\begin{aligned} F(z) = \rho _0 (w_0 + w_a z)(1+z)^{3(1+w_0-w_a)} e^{3 w_a z}. \end{aligned}$$
(26)
Therefore, by using Eq. (23) we obtain
$$\begin{aligned} 4\kappa X(z) = \rho _0^2 ( 1 + w_0 + w_a z)^2 (1+z)^{6(w_0-w_a)} e^{6 w_a z}. \end{aligned}$$
(27)
With these expressions we can plot F(X) parametrically using the scale factor (or the redshift) as the parameter. The values for \(w_0\) and \(w_a\) in the plots are obtained from a test of the model against observational data, in this case a Type Ia supernova. The best fit to the SNIa data gives \(\varOmega _m = 0.2\,\pm \,0.1\), \(w_0 = 0.9\,\pm \,0.1\), and \(w_a = 0.8\,\pm \,0.2\), with \(\chi ^2_\mathrm{red} = 1.23\). In the first panel of Fig. 1 we display F as a function of the redshift z, and in the other X as a function of z. Combining these two functions, we plot in Fig. 2 the reconstructed F(X) using the best fit values of the parameters.
A stability criterion demands that the sound speed be positive \(c_\mathrm{s}^2>0\), which eventually translates into a restriction of the values of the EoS parameter w(z). Using Eq. (7) we notice that \(c_\mathrm{s}^2>0\) means \(X'<0\), or in terms of the derivative with respect to redshift, that \(\mathrm{d}X/\mathrm{d}z>0\). From inspection in Fig. 1 for model A, this never happens in the range \(z\in [0.0,1.6]\). Notice that F(X) is single valued and crosses from negative to positive values around \(X \simeq 0.1\).
The same procedure is performed for the other three parameterizations:
$$\begin{aligned} {\texttt {Model}}~{\texttt {B}}&w(z)= w_0 + w_a z/(1+z) , \nonumber \\ {\texttt {Model}}~{\texttt {C}}&w(z)= w_0 + w_a \ln (1+z) , \nonumber \\ {\texttt {Model}}~{\texttt {D}}&w(z)= w_0 + w_a \ln \left( 1+ z/(1+z) \right) , \end{aligned}$$
(28)
and the results are displayed in Table 1.
Table 1 Summary of the result of the reconstruction for each model
Model B
For model B we have the Chevallier–Polarski–Linder (CPL) parameterization \(w(z)=w_0 + w_a z/(1+z)\). From Eq. (24) we obtain
$$\begin{aligned} \rho (z) = \rho _0 (1+z)^{3(1+w_0+w_a)} \mathrm{e}^{-3 \frac{w_a z}{1+z}}, \end{aligned}$$
(29)
and from Eq. (22) we get
$$\begin{aligned} F(z) = \rho _0 \left( w_0 + \frac{w_a z}{1+z}\right) (1+z)^{3(1+w_0+w_a)} \mathrm{e}^{-3\frac{w_a z}{1+z}}. \end{aligned}$$
(30)
Using Eq. (23) we obtain
$$\begin{aligned} 4k X(z) = \rho _0^2 \left( 1 + w_0 + \frac{w_a z}{1+z}\right) ^2 (1+z)^{6(w_0+w_a)} \mathrm{e}^{-6 \frac{w_a z}{1+z}}. \end{aligned}$$
(31)
Following an identical procedure to the one above, we first plot the expressions for F(z) and X(z) as functions of the redshift (Fig. 3), and then we plot the reconstructed F(X) for the model. The values for \(w_0\) and \(w_a\) in the plots are obtained from a test of the model against observational data (see Table 1). Again, as in the previous case, the model is stable in the entire redshift range. Notice that, as in the previous model, the F(X) function is single valued in the redshift range where the reconstruction is valid (Fig. 4)).
Model C
For model C we work with \(w(z)=w_0 + w_a \ln (1+z)\). From Eq. (24) we obtain
$$\begin{aligned} \rho (z) = \rho _0 (1+z)^{3(1+w_0)+\frac{3}{2}w_a \ln (1+z)} , \end{aligned}$$
(32)
and from Eq. (22) we get
$$\begin{aligned} F(z)= & {} \rho _0 (w_0 + w_a \ln (1+z))\nonumber \\&(1+z)^{3(1+w_0) + \frac{3}{2}w_a \ln (1+z)} . \end{aligned}$$
(33)
Using Eq. (23) we obtain
$$\begin{aligned} 4k X(z)= & {} \rho _0^2 ( 1 + w_0 + w_a \ln (1+z))^2\nonumber \\&(1+z)^{6w_0 + 3w_a \ln (1+z)} . \end{aligned}$$
(34)
As before, we first plot the expressions for F(z) and X(z) as a function of redshift (Fig. 5), and then we plot the reconstructed F(X) for the model. The best fit values for \(w_0\) and \(w_a\) are shown in Table 1. Again, in Fig. 6 we have a completely stable function X(z). Notice that the stability region implies a single-valued F(X) function, as is also the case in Model B and A.
Model D
For model D we work with \(w(z)=w_0 + \ln (1+ \frac{z}{1+z})\). From Eq. (24) we obtain
$$\begin{aligned} \rho (z) = \rho _0 (1+z)^{3(1+w_0)} \mathrm{e}^{g(z)}, \end{aligned}$$
(35)
where g(z) is given by
$$\begin{aligned} g(z)= & {} \frac{\pi ^2w_a}{4}-\frac{3w_a[\ln (1+z)]^2}{2} + 3w_a \text {Li}_2(-1-2z) \nonumber \\&+ 3w_a\ln (2(1+z))\ln (1+2z). \end{aligned}$$
(36)
Here \(\text {Li}_n(z)\) is the ordinary polylogarithmic function [29]. From Eq. (22) we get F(z) and using Eq. (23) we obtain X(z). First we plot the expressions for F(z) and X(z) as functions of the redshift (Fig. 7), and then we plot the reconstructed F(X) for the model. The best fit values of \(w_0\) and \(w_a\) for this model are shown in Table 1. Again, in Fig. 8 in the whole range of z the speed of sound is positive. Although in the previous cases the function X(z) was a increasing function, in this case X(z) decreases with z. This implies that the reconstructed F(X) decreases with X. Notice also that the stability region implies a single-valued F(X) function as is also the case in all the previous cases.