-
The systematic study of one-loop Feynman integrals in perturbative quantum field theories dates back to the end of the 1970s when 't Hooft and Veltman [1] calculated generic one-, two-, three-, and four-point scalar integrals in dimensional regularization (DREG) up to order
ϵ0 , whereϵ=(4−d)/2 with spacetime dimension d. Passarino and Veltman [2] then demonstrated that tensor integrals up to four points can be systematically reduced to scalar ones, and later studies [3, 4] demonstrated that integrals with more than four external legs in4−2ϵ dimensions can be expressed as lower-point ones up to orderϵ0 . These developments in principle solved the problem of next-to-leading order (NLO) calculations for tree-induced scattering processes.The improvements of experimental precision and the progress of theoretical studies require the understanding of scattering amplitudes and cross sections at higher orders in perturbation theory. Hence, we must compute the one-loop integrals to higher orders in
ϵ . These enable us to predict the infrared divergences appearing in two-loop amplitudes [5–13], and they are necessary for computing one-loop squared amplitudes, which are essential ingredients of next-to-next-to-leading order (NNLO) cross sections.Unlike the terms up to order
ϵ0 , generic results for the higher order terms are not available yet. Part of the reason is that integrals with more than four external legs are generally not reducible to lower-point ones when considering higher orders in ϵ. These require further calculations, which are often complicated owing to the increasing number of physical scales involved.It is known [14–16] that one-loop integrals in a given family admit a uniform transcendentality (UT) basis satisfying canonical differential equations of the form [17]
d→f(→x,ϵ)=ϵdA(→x)→f(→x,ϵ),
(1) where
→x is the set of independent kinematic variables, and the matrixdA has thedlog -form:dA(→x)=∑iCidlog(Wi(→x)).
(2) In the above expression,
Ci are matrices consisting of rational numbers, andWi(→x) are algebraic functions of the variables. The functionsWi are called the "letters" for this integral family, and the set of all independent letters is called the "alphabet."At one loop, a canonical basis can be generically constructed by searching for
dlog -form integrands [14–23]. However, obtaining thedlog matrixdA(→x) is not always a trivial task when the number of variables is large. We note that thedlog matrix can be easily reconstructed if we have the knowledge of the alphabet{Wi(→x)} in advance, since the coefficient matricesCi can then be obtained by bootstrapping.Having the alphabet (and hence the matrix
dA(→x) ) in a good form also aids in solving the differential equations (1) order-by-order in the dimensional regulatorϵ . The (suitably normalized) solution can be expressed as a Taylor series:→f(→x,ϵ)=∞∑n=0ϵn→f(n)(→x),
(3) where the nth-order coefficient function can be expressed as a Chen iterated integral [24]:
→f(n)(→x)=∫→x→x0dA(→xn)⋯∫→x2→x0dA(→x1)+→f(n)(→x0).
(4) Such iterated integrals can be analyzed using the language of "symbols" [25–27] that encodes the algebraic properties of the resulting functions. In certain scenarios, these iterated integrals can be solved analytically (either by direct integration or by bootstrapping). The results can often be expressed in terms of generalized polylogarithms (GPLs) [28], which enable efficient numeric evaluation [29–31]. When an analytic solution is not available, they can straightforwardly evaluated numerically through either numerical integration or series expansion [32, 33].
In this paper, we describe a generic method to construct the letters systematically from cut integrals in the Baikov representation [34, 35]. The letters can be generically expressed in terms of various Gram determinants. The letters and symbols of one-loop integrals were considered in [36–39], and our method is similar to that in [37–39]. Nevertheless, we evaluate the cut integrals differently and obtain equivalent but simpler expressions in certain cases utilizing the properties of Gram determinants. Furthermore, we consider the cases of divergent cut integrals, which were ignored in earlier studies. Using our results, all letters for a given integral family can be easily expressed even before constructing the differential equations. These letters will also appear in the corresponding two-loop integrals.
-
We use the method of [16, 23] to construct the canonical basis in the Baikov representation. In this section, we briefly review the construction procedure since it will also be relevant for obtaining the alphabet in the matrices
dA(→x) .Consider a generic one-loop integral topology with
N=E+1 external legs, where E is the number of independent external momenta. Integrals in this topology can be expressed asIa1,⋯,aN=∫ddliπd/21za11za22⋯zaNN,
(5) where
zi are the propagator denominators given byz1=l2−m21,z2=(l+p1)2−m22,⋯,zN=(l+p1+⋯+pE)2−m2N.
(6) Here,
p1,…,pE are external momenta, which we assume to span a space-like subspace of the d-dimensional Minkowski spacetime. This corresponds to the so-called (unphysical) Euclidean kinematics. Results in the physical phase-space region can be defined using analytic continuation.The concept of the Baikov representation involves changing the integration variables from loop momenta
lμ to the Baikov variableszi , and the result is given byIa1,…,aN=1(4π)E/2Γ((d−E)/2)×∫C|GN(z)|(d−E−2)/2|KN|(d−E−1)/2N∏i=1dzizaii,
(7) where
z={z1,…,zN} is the collection of the Baikov variables. The functionGN(z) is a polynomial of the N variables, whileKN is independent ofz . They are given byGN(z)≡G(l,p1,…,pE),KN=G(p1,⋯,pE),
(8) where the Gram determinant is defined as
G(q1,…,qn)≡det
(9) Note that in Eq. (8), the scalar products involving the loop momentum l should be re-expressed in terms of
{\boldsymbol{z}} :\begin{aligned}[b]l^2 =& z_1 + m_0^2 \, , \\ l \cdot p_i =& \frac{z_{i+1} + m_{i+1}^2 - p_i^2 - z_i - m_i^2}{2} - \sum\limits_{j=1}^{i-1} p_i \cdot p_j \, . \end{aligned}
(10) The integration domain
{\cal{C}} in Eq. (7) is determined by the conditionG_N({\boldsymbol{z}})/{\cal{K}}_N \leq 0 with Euclidean kinematics.We are now ready to express the UT integrals
g_N for any N according to [16]. We must distinguish between the cases of odd N and even N:\begin{aligned}[b] g_{N} \big|_{{N\text{-}\rm odd}} =& \frac{\epsilon^{(N+1)/2}}{(4\pi)^{(N-1)/2} \, \Gamma(1-\epsilon)} \\&\times \int \left( -\frac{ {\cal{K}}_N}{G_N({\boldsymbol{z}})} \right)^\epsilon \prod\limits_{i=1}^N \frac{{\rm d} z_i}{z_i} \, , \\ g_{N} \big|_{{N\text{-}\rm even}} =& \frac{\epsilon^{N/2}}{(4\pi)^{(N-1)/2} \, \Gamma(1/2-\epsilon)}\\& \times \int \frac{\sqrt{G_N({\bf{0}})}}{\sqrt{G_N({\boldsymbol{z}})}} \left( -\frac{ {\cal{K}}_N}{G_N({\boldsymbol{z}})} \right)^\epsilon \prod\limits_{i=1}^N \frac{{\rm d} z_i}{z_i} \, , \end{aligned}
(11) where we set
{\cal{K}}_1 = 1 , and 0 means that allz_i 's are zero. Note thatg_{2n-1} andg_{2n} can be naturally identified as Feynman integrals in2n-2\epsilon dimensions:\begin{aligned}[b] g_N \big|_{N=2n-1} =& \epsilon^n \sqrt{ {\cal{K}}_N} \, I_{1 \times N}^{(2n-2\epsilon)} \,, \\ g_N \big|_{N=2n} =& \epsilon^n \sqrt{G_N({\bf{0}})} \, I_{1 \times N}^{(2n-2\epsilon)} \,, \end{aligned}
(12) where
I^{(d)}_{1 \times N} denotes the d-dimensional N-point Feynman integral with all powersa_i = 1 :I^{(d)}_{1 \times N} \equiv \int \frac{{\rm d}^dl}{{\rm i} \pi^{d/2}} \frac{1}{z_1 z_2 \cdots z_N} \,.
(13) They can be related to Feynman integrals in
4-2\epsilon dimensions using dimensional recurrence relations [40, 41]. Applying the above to all sectors of a family, we can build a complete canonical basis satisfying\epsilon -form differential equations. -
Given a basis of Feynman integrals, calculating the derivatives with respect to a kinematic variable
x_i is straightforward. For a UT basis\vec{f}(\vec{x},\epsilon) , we write\frac{\partial}{\partial x_i} \vec{f}(\vec{x},\epsilon) = \epsilon \, {\boldsymbol{A}}_i(\vec{x}\,) \, \vec{f}(\vec{x},\epsilon) \, ,
(14) where the elements in the matrix
{\boldsymbol{A}}_i(\vec{x}) have the property that they contain only simple poles. In principle, we may already attempt to solve these differential equations using direct integration. However, this is often difficult when{\boldsymbol{A}}_i(\vec{x}) contains many irrational functions (square roots). Therefore, a very useful method is to combine the partial derivatives into a total derivative and rewrite the differential equations in the form of Eq. (1). Hence, we must know the alphabet (i.e., the set of independent lettersW_i(\vec{x}) ) in the matrixd{\boldsymbol{A}}(\vec{x}) . With the knowledge of the alphabet, we can easily reconstruct the entire matrixd{\boldsymbol{A}}(\vec{x}) by comparing the coefficients in the partial derivatives.In principle, we may obtain the letters by directly integrating the matrices
{\boldsymbol{A}}_i(\vec{x}) over the variablesx_i and manipulating the resulting expressions. However, in the presence of many square roots (containing high-degree polynomials) in multi-scale problems, these integrations are not easy to perform, and the results are often extremely complicated. Examples are available for various one-loop and multi-loop calculations, e.g., Refs. [42–44]. With such types of expressions, it is highly non-trivial to decide whether a set of letters are independent. There is a package{\texttt{SymBuild}} [45] which can carry out such a task, but the computational burden is rather heavy when there are many square roots. Furthermore, from experience, we know that letters involving square roots can often be expressed in the form\frac{P(\vec{x}) - \sqrt{Q(\vec{x})}}{P(\vec{x}) + \sqrt{Q(\vec{x})}} \, ,
(15) where P and Q are polynomials. Such letters have useful properties under analytic continuation: they are real when
Q(\vec{x}) > 0 and become pure phases whenQ(\vec{x}) < 0 . However, recovering this structure from direct integration is difficult.Given the above considerations, we now describe a novel method of obtaining the letters, particularly those with square roots and multiple scales. Our method is based on the
d\log -form integrals in the Baikov representation under various cuts. We will utilize the generic propagator denominators in Eq. (II) and the Baikov representation (7). Without loss of generality, we define the Baikov cut on the first r variablez_1,\ldots,z_r as [35]\begin{aligned}[b] I_{a_1,\ldots,a_N}\big|_{{r\text{-}\rm cut}} =& \frac{1}{(4 \pi)^{E/2} \, \Gamma((d-E)/2)} \\ & \times \int \prod\limits_{j=r+1}^N \frac{{\rm d} z_j}{z_j^{a_j}} \prod\limits_{i=1}^r \oint_{z_i=0} \frac{{\rm d} z_i}{z_i^{a_i}} \frac{| G_N({\boldsymbol{z}}) |^{(d-E-2)/2}}{|{\cal{K}}_N|^{(d-E-1)/2} } \, . \end{aligned}
(16) An important property of the Baikov cut is that if one of the powers
a_i (1 \leq i \leq r) is non-positive, the cut integral vanishes according to the residue theorem. The coefficient matrices in the differential equations are invariant under the cuts, and we utilize this property to obtain the letters by imposing various cuts.First, we express the differential equation satisfied by an N-point one-loop UT integral
g_N (see Eqs. (11) and (12)) as\begin{aligned}[b] {d} g_N(\vec{x},\epsilon) =& \epsilon \, {d} M_N(\vec{x}) \, g_N(\vec{x},\epsilon) \\& + \epsilon \sum\limits_{m < N} \sum\limits_i {d} M_{N,m}^{(i)}(\vec{x}) \, g_m^{(i)}(\vec{x},\epsilon) \, , \end{aligned}
(17) where
g_N(\vec{x},\epsilon) andg_m^{(i)}(\vec{x},\epsilon) are components of the canonical basis\vec{f}(\vec{x},\epsilon) , while{d} M_N(\vec{x}) anddM_{N,m}^{(i)}(\vec{x}) are entries in the matrixd{\boldsymbol{A}}(\vec{x}) . The above equation clearly indicates that the derivative ofg_N cannot depend on higher-point integrals as well as on other N-point integrals. It may depend on several m-point integrals for eachm < N , and we use a superscript as ing_m^{(i)} anddM_{N,m}^{(i)} to distinguish them. These m-point integrals can be obtained by "squeezing" some of the propagators in the N-point diagram.From Eq. (17), we observe that it is possible to focus on a particular entry of the
d{\boldsymbol{A}} matrix by imposing some cuts. We elaborate on this in the following. In this section, we assume that the master integrals (after imposing cuts) have no divergences such that the integrands can be expanded as Taylor series in\epsilon before integration. We can show that in this scenario, onlyg_N ,g_{N-1}^{(i)} , andg_{N-2}^{(i)} appear on the right side of Eq. (17). We observe that the most complicated letters are given by these cases. Occasionally, we encounter divergences in the cut integrals, and we must expand the integrands as Laurent series in terms of distributions. We discuss these cases in the next section. -
The self-dependent term in Eq. (17) is easy to extract by imposing the "maximal-cut", i.e., cut on all variables
{\boldsymbol{z}} . All the lower-point integrals vanish under this cut, and the differential equation becomesd\tilde{g}_{N}(\vec{x},\epsilon) = \epsilon \, dM_N(\vec{x}) \, \tilde{g}_{N}(\vec{x},\epsilon) \, ,
(18) where
\tilde{g}_N denotes the cut integral. Using the generic form of UT integrals in Eq. (11), we observe thatdM_N(\vec{x}) = d\log \left(-\frac{ {\cal{K}}_N(\vec{x})}{\widetilde{G}_N(\vec{x})}\right) ,
(19) where
\widetilde{G}_N(\vec{x}) \equiv G_N({\bf{0}}) \, .
(20) Hence, the corresponding letter can be selected as
W_N(\vec{x}) = \frac{\widetilde{G}_N(\vec{x})}{ {\cal{K}}_N(\vec{x})} \, .
(21) We note that two letters are equivalent if they only differ by a constant factor or constant power, i.e.,
W(\vec{x}) \sim c \, W(\vec{x}) \sim \left[ W(\vec{x}) \right]^n \, .
(22) Therefore, in practice, we may select a form that is convenient for the particular case at hand.
It is possible that
G_N({\bf{0}}) = 0 such thatW_N(\vec{x}) = 0 and cannot be a letter. In this case, the integral\tilde{g}_{N} itself vanishes under the maximal cut. This means that the integral is reducible to integrals in sub-sectors, and we do not require to consider it as a master integral. -
We now consider the dependence of the derivative of
g_N on sub-sectors withN-1 propagators. We may have N such sub-sectors, corresponding to "squeezing" one of the N propagators. Focusing on one sub-sector integralg_{N-1}^{(i)} , we can always reorganize the propagators (by shifting the loop momentum and relabel the external momenta) such that the squeezed one isz_N . We can then impose a cut on the firstN-1 variables and express the differential equation as\begin{aligned}[b] d\tilde{g}_{N}(\vec{x},\epsilon) =& \epsilon \, dM_{N}(\vec{x}) \, \tilde{g}_{N}(\vec{x},\epsilon) \\& + \epsilon \, dM_{N,N-1}(\vec{x}) \, \tilde{g}_{N-1}(\vec{x},\epsilon) \,,\end{aligned}
(23) where we have suppressed the superscript since only one sub-sector survives the cut. The letter in
dM_{N}(\vec{x}) has been obtained in the previous step, and we now must calculate the letter indM_{N,N-1}(\vec{x}) . -
We first consider the case in which N is an odd number. Using the generic form of one-loop UT integrals Eq. (11), we can write
\begin{aligned}[b]& d\int_{r_-}^{r_+} \left(-\frac{ {\cal{K}}_N}{G_N({\bf{0}}',z_N)}\right)^\epsilon \frac{{\rm d}z_N}{z_N} \\=& \epsilon \, dM_N \int_{r_-}^{r_+} \left(-\frac{ {\cal{K}}_N}{G_N({\bf{0}}',z_N)}\right)^\epsilon \frac{{\rm d}z_N}{z_N} \\ & +dM_{N,N-1} \, \frac{2^{1-2\epsilon} \, \Gamma^2(1-\epsilon)}{ \Gamma(1-2\epsilon)} \left(-\frac{ {\cal{K}}_{N-1}}{\widetilde{G}_{N-1}}\right)^\epsilon \, , \end{aligned}
(24) where the integration boundary is determined by the two roots
r_{\pm} of the polynomialG_N({\bf{0}}',z_N) , and{\bf{0}}' means that the vector{\boldsymbol{z}}'\equiv\{z_1,\ldots,z_{N-1}\} is zero.If both
r_+ andr_- are non-zero, the integration overz_N is convergent for\epsilon \to 0 . We can then set\epsilon = 0 in the equation and obtaindM_{N,N-1} = \frac{1}{2} \, d\int_{r_-}^{r_+} \frac{{\rm d}z_N}{z_N} = \frac{1}{2} \, d\log\frac{r_+}{r_-} \, .
(25) We may already set the letter to
r_+/r_- and stop at this point. However, expressingr_\pm in terms of certain Gram determinants would be useful. This simplifies the procedure to compute the letter and informs us about the physics in the divergent scenariosr_+ = 0 orr_- = 0 .Given the propagator denominators (II) and the definition of the Gram determinant (9), we observe that
z_N only appears in the top-right and bottom-left corners of the Gram matrix. Using the expansion of the determinant in terms of cofactors, we can writeG_N({\bf{0}}',z_N)=-\frac{1}{4} {\cal{K}}_{N-1} z_N^2 - \widetilde{B}_N z_N +\widetilde{G}_N \, ,
(26) where
\widetilde{B}_N \equiv B_N({\bf{0}}) with (recall thatE=N-1 )B_N({\boldsymbol{z}}) \equiv G(l,p_1,\ldots,p_{E-1};\, p_{E},p_1,\ldots,p_{E-1})\, ,
(27) Here, we have defined an extended Gram determinant
\begin{aligned}[b] &G(q_1,\ldots,q_n;\, k_1,\ldots,k_n) \\ =& \det \left( {\begin{array}{*{20}{c}} {{q_1} \cdot {k_1}}&{{q_1} \cdot {k_2}}& \cdots &{{q_1} \cdot {k_n}}\\ {{q_2} \cdot {k_1}}&{{q_2} \cdot {k_2}}&{}& \vdots \\ \vdots &{}& \ddots & \vdots \\ {{q_n} \cdot {k_1}}& \cdots & \cdots &{{q_n} \cdot {k_n}} \end{array}} \right). \end{aligned}
(28) We may further use the geometric picture of Gram determinants to simplify the two roots. The Gram determinants can be expressed as
\begin{aligned}[b] G(q_1,\ldots,q_n) = &\det \left( q_i^\mu q_j^\nu g_{\mu\nu} \right) \\ =& \det(g_{\mu\nu}) \left[ V(q_1,\ldots,q_n) \right]^2 \, , \end{aligned}
(29) where
q_i^\mu is the μth component ofq_i in the subspace spanned by\{q_1,\ldots,q_n\} (with an arbitrary coordinate system), andg_{\mu\nu} is the metric tensor of this subspace.V(q_1,\ldots,q_n) is the volume of the parallelotope formed by the vectorsq_1,\ldots,q_n (in the Euclidean sense).Let
l^\star denote a solution to the equation{\boldsymbol{z}} = 0 (recall thatz_i contains scalar products involving the loop momentum l); we can write\begin{aligned}[b] \widetilde{G}_{N-1} =& G(l^\star,p_1,\ldots,p_{E-1}) \, , \quad \widetilde{G}_N = G(l^\star,p_1,\ldots,p_E) \, , \\ \widetilde{B}_N =& G(l^\star,p_1,\ldots,p_{E-1};\, p_{E},p_1,\ldots,p_{E-1}) \, . \end{aligned}
(30) We let
l^\star_\perp andp_{E\perp} denote the components ofl^\star andp_E perpendicular to the subspace spanned byp_1,\ldots,p_{E-1} , respectively. We are interested in the region in which the subspace of external momenta is space-like, andl^\star_\perp must be time-like (sincel^\star is either time-like or light-like owing to(l^\star)^2 - m_1^2 = 0 ). We can express the components ofl^\star_\perp perpendicular and parallel top_{E\perp} as|l^\star_\perp|\cosh(\eta) and|l^\star_\perp|\sinh(\eta) , respectively, where|l^\star_\perp| \equiv \sqrt{(l^\star_\perp)^2} . We also denote|p_{E\perp}| \equiv \sqrt{-p_{E\perp}^2} . These enables us to write\begin{aligned}[b] \frac{\widetilde{B}_N}{ {\cal{K}}_{N-1}} =& - |l_{\perp}^\star| |p_{E\perp}| \sinh(\eta) \,, \quad \frac{ {\cal{K}}_{N}}{ {\cal{K}}_{N-1}} = -|p_{E\perp}|^2 \,, \\ \frac{\widetilde{G}_N}{ {\cal{K}}_{N-1}} =& -|l_{\perp}^\star|^2 |p_{E\perp}|^2 \cosh^2(\eta) \,, \quad \frac{\widetilde{G}_{N-1}}{ {\cal{K}}_{N-1}} = |l_{\perp}^\star|^2 \,. \end{aligned}
(31) Thus,
\widetilde{B}_N^2 + {\cal{K}}_{N-1} \widetilde{G}_N = - {\cal{K}}_{N-1}^2 |l_{\perp}^\star|^2 |p_{E\perp}|^2 = {\cal{K}}_{N} \widetilde{G}_{N-1} \, .
(32) Note that the above relation can also be obtained from Sylvester's determinant identity applied to Gram determinants (for other applications of this relation, see, e.g., [16, 23, 46]). We encounter further instances of this relation later in this paper.
Expressing
r_\pm in terms of the Gram determinants, we can finally express the letter indM_{N,N-1} (for odd N) asW_{N,N-1}(\vec{x}) = \frac{\widetilde{B}_{N}-\sqrt{\widetilde{G}_{N-1}{\cal{K}}_N}}{\widetilde{B}_{N}+\sqrt{\widetilde{G}_{N-1}{\cal{K}}_N}} \, .
(33) We emphasize that the ingredients
\widetilde{B}_N ,\widetilde{G}_{N-1} , and{\cal{K}}_N can be very complicated functions of the kinematic variables\vec{x} when N and the length of\vec{x} are large, and it is difficult to obtain the letter through direct integration in multi-scale problems.If one of
r_\pm is zero, the integration overz_N is divergent when\epsilon \to 0 , and we cannot expand the integrand as a Taylor series. Actually, we observe thatW_{N,N-1}(\vec{x}) in Eq. (33) becomes zero in this scenario. However, this requires\widetilde{G}_N = 0 , which means thatg_N vanishes under the maximal cut and hence is not a master integral. It is also possible that\widetilde{G}_{N-1} = 0 andg_{N-1} is not a master. In this case,\log W_{N,N-1} = \log(1) = 0 drops out of the differential equations. Therefore, we do not require to consider these cases here. Similar considerations apply to the N-even case, described in the next section. -
We now analyse the scenario in which N is an even number. We proceed similarly as the odd case, and arrive at the cut differential equation
\begin{aligned}[b]& d \int_{r_-}^{r_+} \frac{{\rm d}z_N}{z_N} \frac{\sqrt{\widetilde{G}_N}}{\sqrt{G_N({\bf{0}}',z_N)}} \left[-\frac{ {\cal{K}}_N}{G_N({\bf{0}}',z_N)}\right]^\epsilon \\ \;=& \epsilon \, dM_{N} \int_{r_-}^{r_+} \frac{{\rm d}z_N}{z_N} \frac{\sqrt{\widetilde{G}_N}}{\sqrt{G_N({\bf{0}}',z_N)}} \left[-\frac{ {\cal{K}}_N}{G_N({\bf{0}}',z_N)}\right]^\epsilon \\ &+ 2\pi \, \epsilon \, \frac{2^{2\epsilon} \, \Gamma(1-2\epsilon)}{\Gamma^2(1-\epsilon)} \, dM_{N,N-1} \left(-\frac{ {\cal{K}}_{N-1}}{\widetilde{G}_{N-1}}\right)^\epsilon \, . \end{aligned}
(34) We again assume that the integration over
z_N is convergent for\epsilon \to 0 . We can then expand the integrands on both sides of the above equation. At order\epsilon^0 , the integral on the left side is\int_{r_-}^{r_+} \frac{{\rm d}z_N}{z_N} \frac{\sqrt{\widetilde{G}_N}}{\sqrt{G_N({\bf{0}}',z_N)}} = {\rm i} \pi \, .
(35) Hence, its derivative is zero. Comparing the order
\epsilon^1 coefficients, and plugging in the form ofdM_N obtained earlier in Eq. (19), we obtaindM_{N,N-1} = -\frac{1}{2\pi} \, d \int_{r_-}^{r_+} \frac{{\rm d}z_N}{z_N} \frac{\sqrt{\widetilde{G}_N}}{\sqrt{G_N({\bf{0}}',z_N)}} \log \frac{G_N({\bf{0}}',z_N)}{\widetilde{G}_N} \, .
(36) The above integrand involves multi-valued functions such as square roots and logarithms. To define the integral, we must select a convention including branch cuts for these functions and also the path from
r_- tor_+ . Different conventions will cause results to differ by some constants or an overall minus sign, but these do not affect the letter up to the equivalence mentioned in Eq. (22).We denote
G_N({\bf{0}}',z_N) as(r_+-z_N)(z_N-r_-) {\cal{K}}_{N-1}/4 with{\cal{K}}_{N-1} > 0 , and express the integral as\begin{aligned}[b] M_{N,N-1} =& -\frac{1}{2\pi} \, \int_{r_-}^{r_+} \frac{{\rm d}z_N}{z_N} \sqrt{\frac{r_+ r_-}{(z_N-r_+)(z_N-r_-)}} \\& \times \log \frac{(z_N-r_+)(z_N-r_-)}{r_+ r_-} \, . \end{aligned}
(37) The branch cuts involve the points
r_\pm and\infty on the complexz_N plane. To represent the cuts more clearly, we perform the change of variable:z_N = \frac{1}{t} \,, \quad t_\pm = \frac{1}{r_\mp} \, .
(38) The branch points then become
t_\pm and0 , and we express the integral asM_{N,N-1} = -\frac{1}{2\pi} \int_{t_-}^{t_+} I(t) \, {\rm d}t \, ,
(39) with the integrand
I(t) = \frac{1}{\sqrt{(t-t_+)(t-t_-)}} \left[ \log\frac{t-t_+}{t} + \log\frac{t-t_-}{t} \right] .
(40) With this form of the integrand, we select the branch cut for the square root to be the line segment between
t_+ andt_- , and the branch cuts for the two logarithms to be the line segments between0 andt_\pm , respectively. These branch cuts are depicted as the wiggly lines in Fig. 1, together with several pathsC_{i\pm} thatt lie infinitesimally close to the cuts. We define the square root following the convention that\sqrt{(t-t_+)(t-t_-)} \to t whent \to \infty .We select the integration path in Eq. (39) to along the line segment
{\cal{C}}_{1+} , and express the integral asM_{N,N-1} = -\frac{1}{4\pi} \left[ \int_{{\cal{C}}_{1+}} I(t) \, {\rm d}t - \int_{{\cal{C}}_{1-}} I(t) \, {\rm d}t \right] ,
(41) where we have used the characteristic that the values of
I(t) on{\cal{C}}_{1\pm} differ by a sign. Since no other singularities exist in the complex t plane (including\infty ), we may deform the paths as long as we do not go across the branch cuts. Hence, we know that\begin{aligned}[b] M_{N,N-1} =& \frac{1}{4\pi} \left[ \int_{{\cal{C}}_{2+}} I(t) \, {\rm d}t - \int_{{\cal{C}}_{2-}} I(t) \, {\rm d}t \right] \\ & + \frac{1}{4\pi} \left[ \int_{{\cal{C}}_{3+}} I(t) \, {\rm d}t - \int_{{\cal{C}}_{3-}} I(t) \, {\rm d}t \right]. \end{aligned}
(42) On the paths
{\cal{C}}_{2+} and{\cal{C}}_{2-} , a2\pi {\rm i} difference results from the first logarithm in Eq. (40). A similar difference of-2\pi {\rm i} resulting from the second logarithm occurs between{\cal{C}}_{3+} and{\cal{C}}_{3-} . Therefore, we obtain\begin{aligned}[b] dM_{N,N-1} = &-\frac{\rm i}{2} \, d\int_0^{t_+} \frac{{\rm d}t}{\sqrt{(t-t_+)(t-t_-)}} \\ & - \frac{\rm i}{2} \, d\int_0^{t_-} \frac{{\rm d}t}{\sqrt{(t-t_+)(t-t_-)}} \\ = &-{\rm i} \, d\log \frac{\sqrt{r_+} - \sqrt{r_-}}{\sqrt{r_+} + \sqrt{r_-}} \, . \end{aligned}
(43) Note that with the above convention, we obtain
\begin{aligned}[b]& \int_{r_-}^{r_+} \frac{{\rm d}z_N}{z_N} \frac{\sqrt{\widetilde{G}_N}}{\sqrt{G_N({\bf{0}}',z_N)}}\\ =& \int_{t_-}^{t_+} \frac{{\rm d}t}{\sqrt{(t-t_+)(t-t_-)}} = {\rm i} \pi \, .\end{aligned}
(44) We can now express the roots
r_\pm in terms of Gram determinants. The result can be expressed asdM_{N,N-1} = \frac{\rm i}{2} \, d\log \frac{\widetilde{B}_{N}-\sqrt{-\widetilde{G}_{N} {\cal{K}}_{N-1}}}{\widetilde{B}_{N}+\sqrt{-\widetilde{G}_{N} {\cal{K}}_{N-1}}} \, ,
(45) where the definitions of
\widetilde{B}_{N} ,\widetilde{G}_{N} , and{\cal{K}}_{N-1} are similar as before. Hence, we can express the letter indM_{N,N-1} (for even N) asW_{N,N-1}(\vec{x}) = \frac{\widetilde{B}_{N}-\sqrt{-\widetilde{G}_{N} {\cal{K}}_{N-1}}}{\widetilde{B}_{N}+\sqrt{-\widetilde{G}_{N} {\cal{K}}_{N-1}}} \, .
(46) As mentioned earlier, we do not require to consider the divergent case
\widetilde{G}_{N-1}=0 or the trivial case\widetilde{G}_N=0 here. -
As in the previous subsection, we consider the dependence of the derivative of
g_N on sub-sectors withN-2 propagators. Without loss of generality, we cut on the variables{\boldsymbol{z}}'=\{z_1,\ldots,z_{N-2}\} . Now, we remain with two sub-sectors withN-1 propagators: one with{\boldsymbol{z}}',z_{N-1} and the other with{\boldsymbol{z}}',z_{N} . We use a superscript to distinguish these two, and the differential equation then becomes\begin{aligned}[b] d\tilde{g}_{N} =& \epsilon \Big( dM_{N} \, \tilde{g}_{N} + dM_{N,N-1}^{(1)} \, \tilde{g}_{N-1}^{(1)} \\& + dM_{N,N-1}^{(2)} \, \tilde{g}_{N-1}^{(2)} + dM_{N,N-2} \, \tilde{g}_{N-2} \Big) \, , \end{aligned}
(47) where we have suppressed the arguments of the functions for simplicity.
-
If N is an odd number, assuming convergence and expanding the integrands, we obtain
\begin{aligned}[b] d\int_{\cal{C}} \frac{{\rm d}z_{N-1}}{z_{N-1}}\frac{{\rm d}z_N}{z_N} =& 4\pi \, dM_{N,N-2} \\ &+ 2 \, dM_{N,N-1}^{(1)} \int_{r_-^{(1)}}^{r_+^{(1)}} \frac{{\rm d}z_{N-1}}{z_{N-1}} \frac{\sqrt{\widetilde{G}_{N-1}^{(1)}}}{\sqrt{G_{N-1}^{(1)}({\bf{0}}',z_{N-1})}} \\& + 2 \, dM_{N,N-1}^{(2)} \int_{r_-^{(2)}}^{r_+^{(2)}} \frac{{\rm d}z_N}{z_N} \frac{\sqrt{\widetilde{G}_{N-1}^{(2)}}}{\sqrt{G_{N-1}^{(2)}({\bf{0}}',z_N)}} \,, \end{aligned}
(48) where the domain
{\cal{C}} is determined byG_N({\bf{0}}',z_{N-1},z_N)\geq 0 , andr_{\pm}^{(i)} are the two roots of the polynomialG_{N-1}^{(i)}({\bf{0}}',z) .The two integrals on the right-hand side can be easily performed using Eq. (35), and we obtain
dM_{N,N-2} = dI_{N,N-2} - \frac{\rm i}{2} \left( dM_{N,N-1}^{(1)} + dM_{N,N-1}^{(2)} \right)\, ,
(49) where
I_{N,N-2} is the double integral:I_{N,N-2} = \frac{1}{4\pi} \int_{\cal{C}} \frac{{\rm d}z_{N-1}}{z_{N-1}}\frac{{\rm d}z_N}{z_N} \, .
(50) The integration domain
{\cal{C}} is controlled by the positivity of the polynomial\begin{aligned}[b] G_N({\bf{0}}',z_{N-1}, z_N) =& -\frac{1}{4} {\cal{K}}_{N-1} z_N^2 - B_N({\bf{0}}',z_{N-1},0) \, z_N \\ & + G_N({\bf{0}}',z_{N-1},0) \, . \end{aligned}
(51) The integration over
z_N can be easily performed to yield\begin{aligned}[b] I_{N,N-2} =& \frac{1}{4\pi} \int_{r_{N-1,-}}^{r_{N-1,+}} I(z_{N-1}) \, {\rm d}z_{N-1} \\ \equiv& \frac{1}{4\pi} \int_{r_{N-1,-}}^{r_{N-1,+}} \frac{{\rm d}z_{N-1}}{z_{N-1}} \\ & \times \log \frac{B_N({\bf{0}}',z_{N-1},0) - \sqrt{\Delta(z_{N-1})}}{B_N({\bf{0}}',z_{N-1},0) + \sqrt{\Delta(z_{N-1})}} \,, \end{aligned}
(52) where
r_{N-1,\pm} are the two roots of the polynomialG_{N-1}^{(1)}({\boldsymbol{z}}',z_{N-1}) = G(l,p_1,\ldots,p_{E-1}) \, ,
(53) and
\begin{aligned}[b] \Delta(z_{N-1}) = &\left[ B_N({\bf{0}}',z_{N-1},0) \right]^2 + {\cal{K}}_{N-1} G_N({\bf{0}}',z_{N-1},0) \\ =& {\cal{K}}_N G_{N-1}^{(1)}({\bf{0}}',z_{N-1}) \,. \end{aligned}
(54) We are now interested in the singularities of the integrand
I(z_{N-1}) in Eq. (52). Two poles exist, at0 and\infty , respectively. There is a branch cut betweenr_{N-1,-} andr_{N-1,+} for the square root. There is also a branch cut betweenR_{N-1,-} andR_{N-1,+} for the logarithm, whereR_{N-1,\pm} are the two roots of the polynomialG_N({\bf{0}}',z_{N-1},0) . These singularities are depicted in Fig. 2. We define the integral path of Eq. (52) to be the upper half of the contour{\cal{C}}_1 . Hence, we obtain\begin{aligned}[b] I_{N,N-2} =& \frac{1}{8\pi} \int_{{\cal{C}}_1} I(z_{N-1}) \, {\rm d}z_{N-1} \\ =& -\frac{1}{8\pi} \int_{{\cal{C}}_2+{\cal{C}}_3+{\cal{C}}_4} I(z_{N-1}) \, {\rm d}z_{N-1} \,. \end{aligned}
(55) The integration around
{\cal{C}}_3 is simply(-2\pi{\rm i}) multiplying the residue atz_{N-1} = 0 , i.e.,\begin{aligned}[b] -\frac{1}{8\pi} \, d\int_{{\cal{C}}_3} I(z_{N-1}) \, {\rm d}z_{N-1} =& \frac{\rm i}{4} \, d\log\frac{\widetilde{B}_N - \sqrt{ {\cal{K}}_N \widetilde{G}_{N-1}^{(1)}}}{\widetilde{B}_N + \sqrt{ {\cal{K}}_N \widetilde{G}_{N-1}^{(1)}}} \\ = &\frac{\rm i}{2} dM_{N,N-1}^{(1)} \,. \end{aligned}
(56) On the two sides of
{\cal{C}}_2 , the logarithm differs by2\pi {\rm i} , and\begin{aligned}[b]&-\frac{1}{8\pi} \, d\int_{{\cal{C}}_2} I(z_{N-1}) \, {\rm d}z_{N-1} = \frac{\rm i}{4} \, d\log\frac{R_{N-1,+}}{R_{N-1,-}} \\ = &\frac{\rm i}{4} \, d\log\frac{\widetilde{B}_N - \sqrt{ {\cal{K}}_N \widetilde{G}_{N-1}^{(2)}}}{\widetilde{B}_N + \sqrt{ {\cal{K}}_N \widetilde{G}_{N-1}^{(2)}}} = \frac{\rm i}{2} dM_{N,N-1}^{(2)} \,. \end{aligned}
(57) From the above, we observe that the genuine contribution to
dM_{N,N-2} results only from the integration along{\cal{C}}_4 . For that, we must investigate the behavior of the logarithm in Eq. (52) in the limitz_{N-1} \to \infty . We first note thatG_{N-1}^{(1)}({\bf{0}}',z_{N-1}) \sim - {\cal{K}}_{N-2} z_{N-1}^2 / 4 in that limit. ForB_N({\bf{0}}',z_{N-1},0) , it is a linear function ofz_{N-1} , and the coefficient can be extracted as\begin{aligned}[b] &\frac{\partial B_N({\bf{0}}',z_{N-1},0)}{\partial z_{N-1}} \\ =& \frac{\partial G(l,p_1,\ldots,p_{E-1};\, p_E,p_1,\ldots,p_{E-1})}{\partial z_{N-1}} \\ =& \frac{\partial l \cdot p_E}{\partial z_{N-1}}\frac{\partial G(l,p_1,\ldots,p_{E-1};\, p_E,p_1,\ldots,p_{E-1})}{\partial l \cdot p_E} \\ & + \frac{\partial l \cdot p_{E-1}}{\partial z_{N-1}}\frac{\partial G(l,p_1,\ldots,p_{E-1};\, p_E,p_1,\ldots,p_{E-1})}{\partial l\cdot p_{E-1}} \\ = &\frac{1}{2} G(p_1,\ldots,p_{E-1};\, p_1,\ldots,p_{E-1}) \\ & + \frac{1}{2} G(p_1,\ldots,p_{E-2},p_{E-1};\, p_1,\ldots,p_{E-2},p_{E}) \\ =& \frac{1}{2}G(p_1,\ldots,p_{E-2},p_{E-1};\, p_1,\ldots,p_{E-2},p_{E-1}+p_E) \, . \end{aligned}
(58) Hence, we obtain
\begin{aligned}[b] dM_{N,N-2} =& -\frac{1}{8\pi} \, d\int_{{\cal{C}}_4} I(z_{N-1}) \, {\rm d}z_{N-1} \\ =& \frac{\rm i}{4} d\log \frac{C_N - \sqrt{- {\cal{K}}_N {\cal{K}}_{N-2}}}{C_N + \sqrt{- {\cal{K}}_N {\cal{K}}_{N-2}}} \, , \end{aligned}
(59) where
C_N = G(p_1,\ldots,p_{E-2},p_{E-1};\, p_1,\ldots,p_{E-2},p_{E-1}+p_E) \, .
(60) The letter
W_{N,N-2} can be readily read off. Note that the Gram determinants in this letter only involve external momenta. Hence, the letter has a well-defined limit when\widetilde{G}_{N-2} = 0 andg_{N-2} is not a master. We explain the meaning of this later. -
If N is an even number, assuming no divergence, we obtain the differential equation
d\int_{\cal{C}} \frac{{\rm d}z_{N-1}}{z_{N-1}} \frac{{\rm d}z_N}{z_N}\frac{\sqrt{\widetilde{G}_N}}{\sqrt{G_N({\bf{0}}',z_{N-1},z_N)}} = 4\pi \, dM_{N,N-2} \,,
(61) where the domain
{\cal{C}} is determined byG_N({\bf{0}}',z_{N-1},z_N) \geq 0 . Note that the dependence ong_{N-1}^{(i)} vanishes in this case. We select to integrate overz_N first and obtain\begin{aligned}[b] dM_{N,N-2} =&\frac{1}{4\pi} \, d\int_{r_{N-1,-}}^{r_{N-1,+}} \frac{{\rm d}z_{N-1}}{z_{N-1}} \frac{\sqrt{\widetilde{G}_N}}{\sqrt{G_N({\bf{0}}',z_{N-1},0)}}\end{aligned}
\begin{aligned}[b] \quad\times \int_{r_{N,-}}^{r_{N,+}} \frac{{\rm d}z_N}{z_N}\frac{\sqrt{G_N({\bf{0}}',z_{N-1},0)}}{\sqrt{G_N({\bf{0}}',z_{N-1},z_N)}} \,, \end{aligned}
(62) where
r_{N,\pm} are the two roots of the polynomialG_N({\bf{0}}',z_{N-1},z_N) with respect toz_N (treatingz_{N-1} as a constant). Consequently, the integration range ofz_{N-1} is determined by the discriminant Δ ofG_N({\bf{0}}',z_{N-1},z_N) (with respect to the variablez_N ). Expressing\Delta = {\cal{K}}_4 G_{N-1}^{(1)}\times ({\bf{0}}',z_{N-1}) , we know that the boundsr_{N-1,\pm} are simply the two roots of the polynomialG_{N-1}^{(1)}({\bf{0}}',z_{N-1}) . Here, we define\begin{aligned}[b] G_{N-1}^{(1)}({\boldsymbol{z}}',z_{N-1}) =& G(l,p_1,\ldots,p_{E-1}) \, , \\ G_{N-1}^{(2)}({\boldsymbol{z}}',z_{N}) =& G(l,p_1,\ldots,p_{E-1}+p_E) \, .\end{aligned}
(63) The integration over
z_N can be performed using Eq. (35). We then obtaindM_{N,N-2} = \frac{\rm i}{4} \, dI_{N,N-2} \,,
(64) where
I_{N,N-2} = \int_{r_{N-1,-}}^{r_{N-1,+}} \frac{{\rm d}z_{N-1}}{z_{N-1}} \frac{\sqrt{\widetilde{G}_N}}{\sqrt{G_N({\bf{0}}',z_{N-1},0)}} \, ,
(65) where
r_{N-1,\pm} are the two roots ofG_{N-1}^{(1)}({\bf{0}}',z_{N-1}) . We denote the two roots ofG_N({\bf{0}}',z_{N-1},0) asR_{N-1,\pm} . We can then writeG_N({\bf{0}}',z_{N-1},0) = -\frac{1}{4} {\cal{K}}_{N-1}^{(2)} (z_{N-1}-R_{N-1,+})(z_{N-1}-R_{N-1,-}) \, ,
(66) where
{\cal{K}}_{N-1}^{(2)} = G(p_1,\ldots,p_{E-2},p_{E-1}+p_E) \, .
(67) We define
t = \frac{1}{z_{N-1}} \, , \quad t_{\pm} = \frac{1}{r_{N-1,\mp}} \, , \quad T_{\pm} = \frac{1}{R_{N-1,\mp}} \, .
(68) The integral can then be expressed as
\begin{aligned}[b] I_{N,N-2} =& \int_{t_-}^{t_+} \frac{{\rm d}t}{\sqrt{(t-T_+)(t-T_-)}} \\ =& 2 \log \frac{\sqrt{t_+-T_+} + \sqrt{t_+-T_-}}{\sqrt{t_–T_+} + \sqrt{t_–T_-}} \, . \end{aligned}
(69) We now aim to rewrite the above expression in terms of Gram determinants. Hence, we first write
\begin{aligned}[b] G_N({\bf{0}}',z_{N-1},0) =& -\frac{1}{4} {\cal{K}}_{N-1}^{(2)} z_{N-1}^2 - \widetilde{B}_{N} z_{N-1} + \widetilde{G}_N \, , \\ G_{N-1}^{(1)}({\bf{0}}',z_{N-1}) =& -\frac{1}{4} {\cal{K}}_{N-2} z_{N-1}^2 - \widetilde{B}_{N-1}^{(1)} z_{N-1} + \widetilde{G}_{N-1}^{(1)} \, , \end{aligned}
(70) where
\begin{aligned}[b] {\cal{K}}_{N-2} =& G(p_1,\ldots,p_{E-2}) \, , \\ B_{N-1}^{(1)}({\boldsymbol{z}}) =& G(l,p_1,\ldots,p_{E-2};\, p_{E-1},p_1,\ldots,p_{E-2}) \, . \end{aligned}
(71) The roots are given by
\begin{aligned}[b] t_{\pm} =& \frac{\widetilde{B}_{N-1}^{(1)} \pm \sqrt{ {\cal{K}}_{N-1}^{(1)} \widetilde{G}_{N-2}}}{2\widetilde{G}_{N-1}^{(1)}} \, , \\ T_{\pm} =& \frac{\widetilde{B}_{N} \pm \sqrt{ {\cal{K}}_{N} \widetilde{G}_{N-1}^{(2)}}}{2\widetilde{G}_{N}} \, , \end{aligned}
(72) where
G_{N-1}^{(2)} = G(l,p_1,\ldots,p_{E-2},p_{E-1}+p_E) \, ,
(73) and we have used the relations
\begin{aligned}[b] B_N^2 + {\cal{K}}_{N-1}^{(2)} G_N =& {\cal{K}}_N G_{N-1}^{(2)} \, , \\ \left( B_{N-1}^{(1)} \right)^2 + {\cal{K}}_N G_{N-1}^{(1)} = &{\cal{K}}_{N-1}^{(1)} G_{N-2} \, . \end{aligned}
(74) We can now employ the geometric representations of the Gram determinants in Eq. (31) to simplify the expressions. Let
l^\star be the solution to{\boldsymbol{z}}=0 ; we are interested in the components ofl^\star ,p_{E-1} andp_{E-1}+p_E orthogonal to the subspace spanned by\{p_1,\ldots,p_{E-2}\} . For convenience, we denote these components ask^\mu (forl^\star ),p^\mu (forp_{E-1} ) andq^\mu (forp_{E-1}+p_E ). We note thatk^\mu is time-like, whilep^\mu andq^\mu are space-like. Hence, we can define the norms|k| = \sqrt{k^2} ,|p| = \sqrt{-p^2} , and|q| = \sqrt{-q^2} . We further denote the components ofk^\mu andp^\mu perpendicular to q ask_\perp^\mu andp_\perp^\mu , respectively, and define the corresponding norms as|k_\perp| and|p_\perp| . We can finally writet_{\pm} = \frac{\sinh(\eta_1) \pm {\rm i}}{2 |k| |p| \cosh^2(\eta_1)} \, , \quad T_{\pm} = \frac{\sinh(\eta_2) \pm {\rm i}}{2 |k_{\perp}| |p_\perp| \cosh^2(\eta_2)} \, ,
(75) where
\eta_1 is the hyperbolic angle between k and p, and\eta_2 is the hyperbolic angle betweenk_\perp andp_\perp . It will be convenient to define the imaginary angle\theta_{kp} \equiv \pi/2 - {\rm i}\eta_1 such that\cosh(\eta_1) = \sin\theta_{kp} and{\rm i}\, \sinh(\eta_1) = \cos\theta_{kp} ; similarly,\theta_{kp,\perp q} \equiv \pi/2 - {\rm i}\eta_2 .We use
\theta_{pq} to denote the angle between p and q and define ξ as the hyperbolic angle between k and q (with the corresponding imaginary angle\theta_{kq} \equiv \pi/2 - {\rm i}\xi ). We then obtain the relations\begin{aligned}[b] \quad |p_\perp| =& |p| \sin\theta_{pq} \, , \quad |k_\perp| = |k| \sin\theta_{kq} \, , \\ \cos\theta_{kp} =& \cos\theta_{kq} \cos\theta_{pq} + \cos\theta_{kp,\perp q} \sin\theta_{kq} \sin\theta_{pq} \, . \end{aligned}
(76) Thus,
t_{\pm} - T_{\pm} \equiv \frac{P_{\pm\pm}}{2|k_\perp| |p_\perp| \sin^2\theta_{kp} \sin^2\theta_{kp,\perp q}} \, ,
(77) where
\begin{aligned}[b] P_{\pm\pm} =& (-{\rm i}\cos\theta_{kp} \pm {\rm i}) \sin^2\theta_{kp,\perp q} \sin\theta_{pq} \sin\theta_{kq} \\ &- (-{\rm i}\cos\theta_{kp,\perp q} \pm {\rm i}) \sin^2\theta_{kp} \, .\end{aligned}
(78) Substituting the relation (76), we may express the functions
P_{\pm\pm} as\begin{aligned}[b] P_{++} =& -8 {\rm i} \, \sin^2\left( \frac{\theta_{kp}}{2} \right) \cos^2\left( \frac{\theta_{kq}+\theta_{pq}}{2} \right) \sin^2\left( \frac{\theta_{kp,\perp q}}{2} \right) , \\ P_{+-} =& 8 {\rm i}\, \sin^2\left( \frac{\theta_{kp}}{2} \right) \cos^2\left( \frac{\theta_{kq}-\theta_{pq}}{2} \right) \cos^2\left( \frac{\theta_{kp,\perp q}}{2} \right) , \\ P_{-+} = &-8 {\rm i}\, \cos^2\left( \frac{\theta_{kp}}{2} \right) \sin^2\left( \frac{\theta_{kq}+\theta_{pq}}{2} \right) \sin^2\left( \frac{\theta_{kp,\perp q}}{2} \right) , \\ P_{ - - } =& 8 {\rm i} \, \cos^2\left( \frac{\theta_{kp}}{2} \right) \sin^2\left( \frac{\theta_{kq}-\theta_{pq}}{2} \right) \cos^2\left( \frac{\theta_{kp,\perp q}}{2} \right) . \end{aligned}
(79) Using trigonometry identities together with the relations
\begin{aligned}[b]\cos\theta_{pq} =& \cos\theta_{kp} \cos\theta_{kq} + \cos\theta_{pq,\perp k} \sin\theta_{kp} \sin\theta_{kq} \, , \\ \sin\theta_{pq} =& \sin\theta_{pq,\perp k} \, \frac{\sin\theta_{kp}}{\sin\theta_{kp,\perp q}} \, , \end{aligned}
(80) we obtain a surprisingly simple result:
I_{N,N-2} = 2 \log {\rm e}^{-{\rm i} \theta_{pq,\perp k}} = \log \frac{\cos\theta_{pq,\perp k} - {\rm i} \sin\theta_{pq,\perp k}}{\cos\theta_{pq,\perp k} + {\rm i} \sin\theta_{pq,\perp k}} \, ,
(81) where
\theta_{pq,\perp k} is the angle betweenp_{\perp k} andq_{\perp k} . It is straightforward to rewrite the above expression in terms of Gram determinants, and we finally obtaindM_{N,N-2} = \frac{\rm i}{4} d\log \frac{\widetilde{D}_N - \sqrt{-\widetilde{G}_N\widetilde{G}_{N-2}}}{\widetilde{D}_N + \sqrt{-\widetilde{G}_N\widetilde{G}_{N-2}}} \,,
(82) where
\widetilde{D}_{N} = D_N({\bf{0}}) andD_N({\boldsymbol{z}}) = G(l,p_1,\ldots,p_{E-1};l,p_1,\ldots,p_{E-1}+p_E) \, .
(83) -
In the convergent case,
dg_{N} cannot depend ong_{N-3} or integrals with even fewer propagators. For odd N, this can be easily observed from the powers of\epsilon in Eq. (11). However, for even N,dg_{N} andg_{N-3} are multiplied by the same power of\epsilon in the differential equations. Subsequently, we must examine the three-fold integrals appearing in the differential equations under the(N-3) -cut. The first two folds can be performed using the calculations in Section III.C.2, and the last fold can be studied similar to those in Section III.C.1. Finally, we can arrive at the conclusion thatdM_{N,N-3}=0 in the convergent case. However, note that such dependence can be present in the divergence cases, as discussed in the next section. -
We now consider the scenario in which some cut integrals become divergent and we cannot perform a Taylor expansion for the integrands. As discussed earlier, this occurs when certain Gram determinants vanish under the maximal cut, and the corresponding integrals are reducible to lower sectors. A classical example is the massless three-point integral that can be reduced to two-point integrals. Reducible higher-point integrals can occur with specific configurations of external momenta, which appear, e.g., at boundaries of differential equations or in some effective field theories. Divergent cut integrals can have two types of consequences, which we discuss in the following.
-
We consider the dependence of
dg_{N} ong_{N-2} wheng_{N-1}^{(1)} is reducible, where N is even. Following the derivation in Section III.C.2, we observe that now one ofr_{N-1,\pm} is zero andG_{N-1}^{(1)}({\bf{0}}',0) = 0 . Hence, integration overz_{N-1} is divergent and we cannot perform Taylor expansion of the integrand in\epsilon . Moreover, we observe that the entrydM_{N,N-2} obtained in Section III.C.2 is divergent. To proceed, we can maintain the regulator in the differential equation:\begin{aligned}[b] &d\int_{\cal{C}} \frac{{\rm d}z_{N-1}}{z_{N-1}} \frac{{\rm d}z_N}{z_N} \frac{\sqrt{\widetilde{G}_N}}{\sqrt{G_N({\bf{0}}',z_{N-1},z_N)}} \left[-\frac{ {\cal{K}}_N}{G_N({\bf{0}}',z_{N-1},z_N)}\right]^\epsilon \\ =& \epsilon \, dM_{N} \int_{\cal{C}} \frac{{\rm d}z_{N-1}}{z_{N-1}} \frac{{\rm d}z_N}{z_N} \end{aligned}
\begin{aligned}[b] \quad & \times \frac{\sqrt{\widetilde{G}_N}}{\sqrt{G_N({\bf{0}}',z_{N-1},z_N)}} \left[-\frac{ {\cal{K}}_N}{G_N({\bf{0}}',z_{N-1},z_N)}\right]^\epsilon \\& + 4\pi \, dM_{N,N-2}^\star \left(-\frac{ {\cal{K}}_{N-2}}{\widetilde{G}_{N-2}}\right)^\epsilon + {\cal{O}}(\epsilon) \,, \end{aligned}
(84) where
dM_{N,N-2}^\star denotes the entry in the divergent case. Note thatg_{N-1}^{(1)} is not a master integral and does not contribute to the right-hand side, while the last{\cal{O}}(\epsilon) denotes a suppressed contribution from another(N-1) -point integralg_{N-1}^{(2)} . Here, we assume thatG_{N-1}^{(2)}({\bf{0}}',0) is non-zero and the integration overz_N is convergent for\epsilon \to 0 .We now must perform Laurent expansions of the integrands in terms of distributions. We write
\begin{aligned}[b] G_{N-1}^{(1)}({\bf{0}}',z_{N-1}) =& \frac{1}{4} {\cal{K}}_{N-2} z_{N-1} \, (t - z_{N-1}) \, , \\ t =& - \frac{4\widetilde{B}_{N-1}^{(1)}}{ {\cal{K}}_{N-2}} \, . \end{aligned}
(85) We can then use
\int_0^t \frac{{\rm d}z}{z^{1+\epsilon}} \, f(z) = -\frac{t^{-\epsilon}}{\epsilon} \, f(0) + \int_0^t \frac{{\rm d}z}{z^{1+\epsilon}} \left[ f(z) - f(0) \right] ,
(86) to perform the series expansion. In particular, we obtain
\begin{aligned}[b]&\int_{\cal{C}} \frac{{\rm d}z_{N-1}}{z_{N-1}} \frac{{\rm d}z_N}{z_N} \frac{\sqrt{\widetilde{G}_N}}{\sqrt{G_N({\bf{0}}',z_{N-1},z_N)}} \left[-\frac{ {\cal{K}}_N}{G_N({\bf{0}}',z_{N-1},z_N)}\right]^\epsilon \\ =& {\rm i}\pi \int_0^t \frac{{\rm d}z_{N-1}}{z_{N-1}^{1+\epsilon}} \frac{\sqrt{\widetilde{G}_N}}{\sqrt{G_N({\bf{0}}',z_{N-1},0)}} \\&\times \left[ 1 + \epsilon \, h(z_{N-1}) + {\cal{O}}(\epsilon^2) \right] \\ =& {\rm i}\pi \Bigg[ -\frac{1}{\epsilon} + \log(t) - h(0) \\& + \int_0^t \frac{{\rm d}z_{N-1}}{z_{N-1}} \left( \frac{\sqrt{\widetilde{G}_N}}{\sqrt{G_N({\bf{0}}',z_{N-1},0)}} - 1 \right) \Bigg] + {\cal{O}}(\epsilon) \, , \end{aligned}
(87) where the function
h(z_{N-1}) results from the expansion in\epsilon after integrating overz_N . Whenz_{N-1} \to 0 , it reduces toh(0) = \log \left( \frac{4 {\cal{K}}_{N-1}^{(1)}}{\widetilde{B}_{N-1}^{(1)}} \right) + 4\log(2) \, .
(88) The last integral in Eq. (87) can be obtained by obtaining the limit
\widetilde{G}_{N-1}^{(1)} \to 0 in the difference between Eq. (82) and a simple integral of1/z_{N-1} :\begin{aligned}[b]& \int_0^t \frac{{\rm d}z_{N-1}}{z_{N-1}} \left( \frac{\sqrt{\widetilde{G}_N}}{\sqrt{G_N({\bf{0}}',z_{N-1},0)}} - 1 \right) \\ =& \lim\limits_{\widetilde{G}_{N-1}^{(1)} \to 0} \left( \log\frac{\widetilde{D}_{N} - \sqrt{-\widetilde{G}_{N} \widetilde{G}_{N-2}}}{\widetilde{D}_{N} + \sqrt{-\widetilde{G}_{N} \widetilde{G}_{N-2}}} - \log\frac{\widetilde{B}_{N-1}^{(1)} +\sqrt{\widetilde{G}_{N-2} {\cal{K}}_{N-1}^{(1)}}}{\widetilde{B}_{N-1}^{(1)} -\sqrt{\widetilde{G}_{N-2} {\cal{K}}_{N-1}^{(1)}}} \right) \,. \end{aligned}
(89) Using the relations
\begin{aligned}[b] -G_{N} G_{N-2}=&D_{N}^2-G_{N-1}^{(1)}G_{N-1}^{(2)} \, , \\ G_{N-2} {\cal{K}}_{N-1}^{(1)}=&\left(B_{N-1}^{(1)}\right)^2+G_{N-1}^{(1)} {\cal{K}}_{N-2} \, , \end{aligned}
(90) we can simplify the expression and obtain
\int_0^t \frac{{\rm d}z_{N-1}}{z_{N-1}} \left( \frac{\sqrt{\widetilde{G}_N}}{\sqrt{G_N({\bf{0}}',z_{N-1},0)}} - 1 \right) = \log \frac{\widetilde{G}_N {\cal{K}}_{N-2}}{ {\cal{K}}_{N-1}^{(1)}\widetilde{G}_{N-1}^{(2)} } \, .
(91) Now, we can combine everything, and we observe that in the divergent case (for even N),
W_{N,N-2}^\star = \frac{\widetilde{G}_{N-2} \, {\cal{K}}_N}{ {\cal{K}}_{N-1}^{(1)} \, \widetilde{G}_{N-1}^{(2)}} \, .
(92) Comparing to Eq. (92), we note that the letter in the divergent case is simpler (without square roots) than that in the convergent case. Interestingly, this simple letter can be obtained without using the tedious calculation above. We observe that in the divergent case
\widetilde{G}_{N-1}^{(1)} \to 0 , we have the relation\tilde{g}_{N-1}^{(1)} = -\frac{1}{2} \tilde{g}_{N-2} \, .
(93) This hints that we should combine
dM_{N,N-1}^{(1)} anddM_{N,N-2} to obtaindM_{N,N-2}^\star :\begin{aligned}[b] dM_{N,N-2}^{\star} =& \lim\limits_{\widetilde{G}_{N-1}^{(1)}\to 0} \left( -\frac{1}{2} dM_{N,N-1}^{(1)} + dM_{N,N-2} \right) \\ =& \frac{\rm i}{4} \lim\limits_{\widetilde{G}_{N-1}^{(1)} \to 0} \left( \log\frac{\widetilde{D}_{N} - \sqrt{-\widetilde{G}_{N} \widetilde{G}_{N-2}}}{\widetilde{D}_{N} + \sqrt{-\widetilde{G}_{N} \widetilde{G}_{N-2}}} \right.\\&-\left. \log\frac{\widetilde{B}_{N}^{(1)} -\sqrt{-\widetilde{G}_{N} {\cal{K}}_{N-1}^{(1)}}}{\widetilde{B}_{N}^{(1)} +\sqrt{-\widetilde{G}_{N} {\cal{K}}_{3}^{(N)}}} \right) \,. \end{aligned}
(94) Using the relations in Eq. (90) as well as
-G_{N} {\cal{K}}_{N-1}^{(1)}=\left(B_{N}^{(1)}\right)^2+G_{N-1}^{(1)} {\cal{K}}_{N} \, ,
(95) we can easily arrive at Eq. (92).
Further divergences may occur if
\widetilde{G}_{N-1}^{(2)} = 0 in Eq. (92). In this case, bothg_{N-1}^{(1)} andg_{N-1}^{(2)} are reducible to lower-point integrals. The corresponding letter can be obtained by includingdM_{N,N-1}^{(2)} , but we do not elaborate on the calculation here. We finally note that the above considerations can also be applied to the N-odd cases, although hereg_{N-1}^{(i)} can only be reducible for specific configurations of external momenta. We discuss similar scenarios in the next subsection. -
In the convergent case, we have observed that
dg_{N} can only depend ong_N ,g_{N-1}^{(i)} , andg_{N-2}^{(i)} . This picture changes in the divergent case when one ofg_{N-2}^{(i)} is reducible, anddg_{N} may develop dependence on some(N-3) -point integrals. As a practical example, we consider the dependence of 5-point integrals on 2-point ones. According to Eq. (17), we obtain\begin{aligned}[b] d\tilde{g}_5 =& \epsilon \, dM_5 \, \tilde{g}_5 + \epsilon \sum\limits_i dM_{5,4}^{(i)} \, \tilde{g}_4^{(i)} + \epsilon \sum\limits_i dM_{5,3}^{(i)} \, \tilde{g}_3^{(i)} \\ & + \epsilon \, dM_{5,2} \, \tilde{g}_2 \, , \end{aligned}
(96) where the cut on
z_1 andz_2 is imposed. Using Eq. (11), we arrive at\begin{aligned}[b] dM_{5,2} + {\cal{O}}(\epsilon) =& \frac{\epsilon}{8\pi} \, dI_{5,2}(\epsilon) - \frac{\epsilon}{4\pi} \sum\limits_{i=3}^5 dM_{5,4}^{(i)} \, I_{4,2}^{(i)}(\epsilon) \\ &- \frac{\epsilon}{2} \sum\limits_{i=3}^5 dM_{5,3}^{(i)} \, I_{3,2}^{(i)}(\epsilon) \, , \end{aligned}
(97) where
\begin{aligned}[b] I_{5,2}(\epsilon) =& \int \frac{{\rm d}z_3}{z_3} \frac{{\rm d}z_4}{z_4} \frac{{\rm d}z_5}{z_5} \left( -\frac{ {\cal{K}}_5}{G_5(0,0,z_3,z_4,z_5)} \right)^\epsilon , \\ I_{4,2}^{(i)}(\epsilon) =& \int \frac{{\rm d}z_j}{z_j} \frac{{\rm d}z_k}{z_k} \frac{\sqrt{G_4^{(i)}(0,0,0,0)}}{\sqrt{G_4^{(i)}(0,0,z_j,z_k)}} \\& \times \left( -\frac{ {\cal{K}}_4^{(i)}}{G_4^{(i)}(0,0,z_j,z_k)} \right)^\epsilon , \\ I_{3,2}^{(i)}(\epsilon) =& \int \frac{{\rm d}z_i}{z_i} \left( -\frac{ {\cal{K}}_3^{(i)}}{G_3^{(i)}(0,0,z_i)} \right)^\epsilon , \end{aligned}
(98) where
j<k andj,k \neq i . We note that each term on the right-hand side of Eq. (97) has a factor of\epsilon . Therefore, the term can only contribute if the integral is divergent in the limit\epsilon \to 0 . For that to occur, at least one ofG_3^{(i)}(0,0,0) must vanish. For simplicity, we assumeG_3^{(3)}(0,0,0) = 0 , while the other twoG_3^{(i)}(0,0,0) 's are non-zero. Generally, it is clear that theI_{3,2}^{(i)}(\epsilon) terms do not contribute since they are either zero or non-divergent. The integralsI_{4,2}^{(4)}(\epsilon) andI_{4,2}^{(5)}(\epsilon) are similar to Eq. (87) with the result-{\rm i}\pi/\epsilon + {\cal{O}}(\epsilon^0) . Therefore, we only require to address the divergent part ofI_{5,2}(\epsilon) :\begin{aligned}[b] I_{5,2}(\epsilon) =& \int \frac{{\rm d}z_3}{z_3} \frac{{\rm d}z_4}{z_4} \left[ \Delta(z_3,z_4) \right]^{-\epsilon} \\& \times\log\frac{B_5^{(5)}(0,0,z_3,z_4,0) - \sqrt{\Delta(z_3,z_4)}}{B_5^{(5)}(0,0,z_3,z_4,0) + \sqrt{\Delta(z_3,z_4)}} + {\cal{O}}(\epsilon^0) \, , \end{aligned}
(99) where
\Delta(z_3,z_4) = {\cal{K}}_5 G_{4}^{(5)}(0,0,z_3,z_4) \, .
(100) The integration over
z_4 is similar to Eq. (52), except for the additional factor\Delta^{-\epsilon} , which regularizes the divergence asz_3 \to 0 . Since we are only interested in the leading term in\epsilon , it is equivalent to replacing this factor byz_3^{-\epsilon} . We can then expandz_3^{-1-\epsilon} in terms of distributions. Maintaining only the1/\epsilon terms, we obtain\begin{aligned}[b] &dI_{5,2}(\epsilon) + {\cal{O}}(\epsilon^0)\\ =& -\frac{1}{\epsilon} d\int \frac{{\rm d}z_4}{z_4} \log\frac{B_5^{(5)}(0,0,0,z_4,0) - \sqrt{\Delta(0,z_4)}}{B_5^{(5)}(0,0,0,z_4,0) + \sqrt{\Delta(0,z_4)}} \\ =& -\frac{1}{\epsilon}\left( 2\pi {\rm i} \, dM_{5,4}^{(4)} + 2\pi {\rm i}\, dM_{5,4}^{(5)} + 4\pi \, dM_{5,3}^{(3)} \right)\, , \end{aligned}
(101) where the second line follows from the calculation of Eq. (52). We finally arrive at
dM_{5,2} = -\frac{1}{2} dM_{5,3}^{(3)} = -\frac{\rm i}{8} d\log \frac{C_5 - \sqrt{- {\cal{K}}_5 {\cal{K}}_{3}}}{C_5 + \sqrt{- {\cal{K}}_5 {\cal{K}}_{3}}} ,
(102) where
C_5 = G(p_1,p_2,p_3,p_4;\, p_1,p_2,p_3,p_4+p_5) \, .
(103) The result in Eq. (102) is unsurprising owing to the relation
g_3^{(3)}=-g_2/2 . Similar behaviors are observed when more than one\widetilde{G}_3 vanish. The correspondingdM_{5,2} is then a linear combination of severaldM_{5,3} 's. Hence, we conclude that letters in these cases can also be obtained straightforwardly without tedious calculations.The above discussion relates the appearance of
dM_{N,N-3} to the reducibility of one or moreg_{N-2}^{(i)} 's. We may consider that, if in addition, one or moreg_{N-3}^{(i)} 's becomes reducible,dM_{N,N-4} can appear in the differential equations. This is impossible for integrals with generic external momenta (i.e., the E external momenta are indeed independent). However, such cases may occur at certain boundaries of kinematic configurations. When this occurs, the corresponding letters can be easily obtained using the reduction rules among the integrals, as is conducted in the previous paragraph. -
In summary, we have studied the alphabet for one-loop Feynman integrals. The alphabet governs the form of the canonical differential equations and provides important information on the analytic solution of these equations. We observe that the letters in the alphabet can be generically constructed using UT integrals in the Baikov representation under various cuts. We have first considered cases in which all the cut integrals are convergent in the limit
\epsilon \to 0 . The corresponding letters coincide with the results in [37–39], while our expressions are simpler in certain cases. We have also thoroughly studied the cases of divergent cut integrals. We observe that letters in the divergent cases can be easily obtained from the convergent cases by applying certain limits. The letters admit universal expressions in terms of various Gram determinants. We have checked our general results for several known examples and observed agreements. We have also applied our results to the complicated case of a2 \to 3 amplitude with seven physical scales. The details of that is presented in Ref. [44].We expect that our results will be useful in many calculations of
2 \to 3 and2 \to 4 amplitudes, which are theoretically and/or phenomenologically interesting. It is also interesting to observe whether similar universal structures can be obtained at higher loop orders using the UT integrals in the Baikov representation of [16, 23].
Alphabet of one-loop Feynman integrals
- Received Date: 2022-03-04
- Available Online: 2022-09-15
Abstract: In this paper, we present the universal structure of the alphabet of one-loop Feynman integrals. The letters in the alphabet are calculated using the Baikov representation with cuts. We consider both convergent and divergent cut integrals and observe that letters in the divergent cases can be easily obtained from convergent cases by applying certain limits. The letters are written as simple expressions in terms of various Gram determinants. The knowledge of the alphabet enables us to easily construct the canonical differential equations of the