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Jacobi Elliptic Functions and the
Complete Solution to the Bead on the Hoop Problem

Thomas E. Baker    Andreas Bill Andreas.Bill$@$csulb.edu; author to whom correspondence should be addressed. California State University Long Beach, Department of Physics & Astronomy, 1250 Bellflower Blvd., Long Beach, CA 90840
(submitted June 13, 2011)
Abstract

Jacobi elliptic functions are flexible functions that appear in a variety of problems in physics and engineering. We introduce and describe important features of these functions and present a physical example from classical mechanics where they appear: a bead on a spinning hoop. We determine the complete analytical solution for the motion of a bead on the driven hoop for arbitrary initial conditions and parameter values.

I Introduction

In 1788, James Watt introduced a mechanical device into steam engines that moderated the flow of steam and controlled the speed of the engine.Hart49 ; Dickinson67 This device, known as the governor, is composed of two solid pendula (weights) fixed to a common vertical axis. The power of the steam engine rotates the axis and lifts the weights to a height determined by the angular speed. The behavior of the weights is nowadays presented to students as an example of Lagrangian mechanics as a mass constrained to move frictionlessly on the surface of a sphere with constant azimuthal frequency or a bead moving on a rotating hoop.Goldstein02 ; Taylor05

Solving the equation of motion of the bead on a rotating hoop is generally avoided as it does not have a straightforward solution. The problem is usually limited to the determination of the stationary position of the mass for a given angular frequency of the hoop, although some papers treat the complete problem numerically or within some approximations.Whittaker37 ; Bowman53 ; Lima10 Here, we present the full analytical solution for the motion of the bead on the hoop which requires the use of Jacobi elliptic functions (JEFs).

There are a number of physics problems where JEFs provide an excellent approximation if not a complete description of the system.Erdos00 ; Fu01 These special functions are also amply used in the conformal mapping of engineering problems.Bowman53 ; Kinnersley JEFs have some interesting features. For example, trigonometric and hyperbolic functions are special cases of Jacobi elliptic functions. If considered in the complex plane, JEFs are doubly periodic, a feature appearing, for example, in bifurcation theory of chaotic systems.Ochoa06

Despite the diversity of physical problems where JEFs appear, these functions are generally not part of the physics curriculum. This motivates us to offer a concise and pedagogical exposition of these functions. We then demonstrate how these special functions appear in the example of the bead on the hoop.

II Introducing Jacobi Elliptic functions

In this section, we introduce Jacobi elliptic functions through elliptic geometry and integral inversion,Bowman53 ; Baker1906 ; Armitage06 ; Prasolov97 ; Chandrasekharan85 ; Neville71 and discuss the geometrical interpretation of their arguments.

II.1 Definitions and relations between Jacobi elliptic functions

We start by redefining the basic trigonometric functions sine and cosine in terms of the functional inverse of specific integrals. Usually, these functions are introduced using circular geometry. That is, for a given point (x,y)(x,y) on a circle of radius rr, sinθ=y/r\sin\theta=y/r and cosθ=x/r\cos\theta=x/r. An alternative way to define these functions is to realize that each inverse trigonometric function is a solution of a definite integral. For example, simple trigonometric substitutions lead to

0ydt1t2=arcsiny,0ydt1+t2=arctany,\displaystyle\int_{0}^{y}\frac{dt}{\sqrt{1-t^{2}}}=\arcsin y,\quad\int_{0}^{y}\frac{dt}{1+t^{2}}=\arctan y, (1)

with the conditions that 1y1-1\leq y\leq 1 and 1t20\sqrt{1-t^{2}}\geq 0. We can reinterpret these relations by stating that they define the inverse trigonometric functions. Following Abel we obtain trigonometric functions by inverting these integrals.Prasolov97 For example, defining the argument θ\theta as

θ(y)=0ydt1t2=arcsiny,\theta(y)=\int_{0}^{y}\frac{dt}{\sqrt{1-t^{2}}}=\arcsin y, (2)

we obtain the trigonometric sine function sinθ=y\sin\theta=y. With the Pythagorean relation, we can define the cosine function and all others follow. This alternative definition implies that the integrals θ(y)\theta(y) must in particular display the parity and periodicity of the corresponding trigonometric functions y(θ)y(\theta).

Consider now the case of elliptic geometry. Gauss, Legendre, Abel, Jacobi and Weierstrass studied in depth properties of elliptic functions and integrals. For the purpose of this paper we note only the result, proved by Legendre,Baker1906 that any integrated expression containing a third or fourth degree polynomial in the denominator of a fraction can be reduced to a linear combination of the following elliptic integrals of the first, second, and third kind,

F(y,k)\displaystyle F\left(y,k\right) =\displaystyle= 0ydt(1t2)(1k2t2)\displaystyle\int_{0}^{y}\dfrac{dt}{\sqrt{\left(1-t^{2}\right)\left(1-k^{2}t^{2}\right)}}
F(ϕ,k)\displaystyle F\left(\phi,k\right) =\displaystyle= 0ϕdϕ1k2sin2ϕ\displaystyle\int_{0}^{\phi}\dfrac{d\phi^{\prime}}{\sqrt{1-k^{2}\sin^{2}\phi^{\prime}}} (3)
E(y,k)\displaystyle E\left(y,k\right) =\displaystyle= 0y1k2t21t2𝑑t\displaystyle\int_{0}^{y}\sqrt{\dfrac{1-k^{2}t^{2}}{1-t^{2}}}dt
E(ϕ,k)\displaystyle E\left(\phi,k\right) =\displaystyle= 0ϕ1k2sin2ϕ𝑑ϕ\displaystyle\int_{0}^{\phi}\sqrt{1-k^{2}\sin^{2}\phi^{\prime}}\,d\phi^{\prime} (4)
Π(y,k,n)\displaystyle\Pi\left(y,k,n\right) =\displaystyle= 0ydt(1n2t2)(1t2)(1k2t2)\displaystyle\int_{0}^{y}\dfrac{dt}{\left(1-n^{2}t^{2}\right)\sqrt{\left(1-t^{2}\right)\left(1-k^{2}t^{2}\right)}}
Π(ϕ,k,n)\displaystyle\Pi\left(\phi,k,n\right) =\displaystyle= 0ϕdϕ(1n2sin2ϕ)1k2sin2ϕ,\displaystyle\int_{0}^{\phi}\frac{d\phi^{\prime}}{\left(1-n^{2}\,\sin^{2}\phi^{\prime}\right)\sqrt{1-k^{2}\,\sin^{2}\phi^{\prime}}}, (5)

where y=sinϕy=\sin\phi, t=sinϕt=\sin\phi^{\prime}, k(1,1)k\in(-1,1) is the modulus and nn\in\mathbb{R} the characteristic. We assume all square roots to be positive. In Eqs. (II.1)–(II.1), the first expression (in tt) is known as the Jacobi form whereas the second (in ϕ\phi^{\prime}) is Legendre’s form. When ϕ=π/2\phi=\pi/2, written F(π2,k)K(k)F\left(\tfrac{\pi}{2},k\right)\equiv K\left(k\right), the integrals are said to be complete and otherwise incomplete. We will use the first two elliptic integrals exclusively in what follows.

Because trigonometric functions are sometimes more useful than their inverses, it may be worthwhile to invert the elliptic integrals as well.Bowman53 ; Prasolov97 In this process, Abel and Jacobi followed the work of Legendre and introduced what are now known as the Jacobi elliptic functions. These functions result from the inversion of the elliptic integral of the first kind. Introducing the Jacobi notation u(ϕ)F(ϕ,k)u(\phi)\equiv F(\phi,k) for this integral, we can formally invert the Legendre form of the integral, Eq. (II.1), to obtain ϕ(u)=amu\phi(u)=\mathrm{am}\,u, the amplitude of uu. In the Jacobi form, u(y)=F(y,k)u(y)=F(y,k), the inversion of Eq. (II.1) leads one to define the sine-amplitude Jacobi elliptic function written in Glaisher’s notation (y[1,1]y\in[-1,1], ϕ[π/2,π/2]\phi\in[-\pi/2,\pi/2])

sn(u,k)y=sinϕ=sin(amu).\mathrm{sn}(u,k)\equiv y=\sin\phi=\sin\left(\mathrm{am}\,u\right). (6)

Note that the kk-dependence is often implicit in the literature, resulting in the notation snu\mathrm{sn}\,u instead of sn(u,k)\mathrm{sn}\left(u,k\right). The last two equalities in Eq. (6) relate the Legendre and Jacobi forms of the elliptic integrals and justify the name given to this Jacobi elliptic function. Because Eq. (II.1) is odd, u(y)=F(y,k)=sn1(y,k)u(y)=F(y,k)=\mathrm{sn}^{-1}(y,k) is odd in yy as well. That is, the sine-amplitude is an odd function of uu.

It is natural to introduce two further Jacobi elliptic functions. Taking the cosine of the amplitude of uu, we define the cosine-amplitude

cn(u,k)cosϕ=cos(amu).\mathrm{cn}(u,k)\equiv\cos\phi=\cos\left(\mathrm{am}\,u\right). (7)

An alternative way to define this function is to write cnu1sn2u\mathrm{cn}\,u\equiv\sqrt{1-\mathrm{sn}^{2}u} since, from Eq. (6), y[1,1]y\in[-1,1].

Finally, in the Legendre form all elliptic integrals in Eqs. (II.1)–(II.1) contain Δ(ϕ)1k2sinϕ\Delta(\phi)\equiv\sqrt{1-k^{2}\,\sin\phi}. This leads one to define the delta-amplitude JEF that can also be written as a derivative of the amplitudeNeville71

dn(u,k)1k2sn2u=d(amu)du.\mathrm{dn}(u,k)\equiv\sqrt{1-k^{2}\mathrm{sn}^{2}u}=\frac{d(\mathrm{am}u)}{du}. (8)

Equation (II.1) can also be used to obtain the last equality. Figure 1 displays the characteristic behavior of the sine-, cosine- and delta-amplitude functions.

Refer to caption
Figure 1: (Color online) Representative graphs of the Jacobi elliptic functions sn(u)(u), cn(u)(u), and dn(u)(u) at fixed value of the modulus k=0.9k=0.9. In the bead and the hoop problem, that argument is a function of time.

From the definitions above immediately follow the identities

sn2u+cn2u\displaystyle\mathrm{sn}^{2}u+\mathrm{cn}^{2}u =\displaystyle= 1,\displaystyle 1, (9)
dn2u+k2sn2u\displaystyle\mathrm{dn}^{2}u+k^{2}\,\mathrm{sn}^{2}u =\displaystyle= 1,\displaystyle 1, (10)
cn2u+(1k2)sn2u\displaystyle\mathrm{cn}^{2}u+(1-k^{2})\,\mathrm{sn}^{2}u =\displaystyle= dn2u.\displaystyle\mathrm{dn}^{2}u. (11)

For limiting values of kk, the Jacobi elliptic functions reduce to trigonometric and hyperbolic functions

k\displaystyle k =\displaystyle= 0:snu=sinu,cnu=cosu,dnu=1,\displaystyle 0:\,\,\mathrm{sn}u=\sin\,u,\,\,\mathrm{cn}\,u=\cos\,u,\,\,\mathrm{dn}u=1, (12)
k\displaystyle k =\displaystyle= 1:snu=tanhu,cnu=dnu=sechu.\displaystyle 1:\,\,\mathrm{sn}u=\tanh\,u,\,\,\mathrm{cn}\,u=\mathrm{dn}u=\mathrm{sech}\,u. (13)

Jacobi elliptic functions thus include trigonometric and hyperbolic functions as special cases. However, JEFs are more than a simple generalization of elementary functions as can be seen when studying the properties of these functions in the complex plane (see Appendix A).

Finally, we mention that from the definitions (6)–(8), one can define quotients of JEFs. One defines scu=snu/cnu\mathrm{sc}\,u=\mathrm{sn}\,u/\mathrm{cn}\,u which carries the name tangent-amplitude scutnu\mathrm{sc}\,u\equiv\mathrm{tn}\,u. Other quotients are, for example, ndu=1/dnu\mathrm{nd}\,u=1/\mathrm{dn}\,u, sdu=snu/dnu\mathrm{sd}\,u=\mathrm{sn}\,u/\mathrm{dn}\,u, etc. Further properties of JEFs that are used in the treatment of the bead on the hoop are summarized in Appendix A.

II.2 Geometric interpretation of the arguments (u,k)(u,k)

In the case of trigonometric functions, such as y=sinθy=\sin\theta, the argument θ\theta has an unequivocal geometric interpretation in circular geometry; it is the angle between the xx-axis and the radius at a specific point (x,y)(x,y) on the circle. The question arises whether in a JEF the argument uu and the modulus kk have a geometric meaning as well. We first caution that the argument of a special function (Bessel, Hypergeometric, etc.) does not generally have such unequivocal physical or geometric meaning. For JEFs, the geometric definition of the argument kk is unique but not for the argument uu, an important point not discussed explicitly in the literature.

The modulus kk is given in elliptic geometry by k=ϵk=\epsilon, the eccentricity of the ellipse ϵ2=1b2/a2\epsilon^{2}=1-b^{2}/a^{2}, where a>ba>b are the semi-axes (see Fig. 2)

x2a2+y2b2=1.\frac{x^{2}}{a^{2}}+\frac{y^{2}}{b^{2}}=1. (14)

The equivalence between kk and ϵ\epsilon is found by realizing that the arc length sBPs_{BP} on the ellipse is expressed in terms of the elliptic integral of the second kind. Using the parametrization x=asinϕx=a\,\sin\phi, y=bcosϕy=b\,\cos\phi, the infinitesimal arc length along the ellipse is

ds\displaystyle ds =\displaystyle= dx2+dy2=a2cos2ϕ+b2sin2ϕdϕ\displaystyle\sqrt{{dx}^{2}+{dy}^{2}}=\sqrt{a^{2}\cos^{2}\phi+b^{2}\sin^{2}\phi}\,\,d\phi (15)
=\displaystyle= a1ϵ2sin2ϕdϕ.\displaystyle a\sqrt{1-\epsilon^{2}\sin^{2}\phi}\,\,d\phi.

Using Eq. (II.1), the arc length sBPs_{BP} of the ellipse from BB to PP can be written

sBP=a0ϕ1ϵ2sin2ϕ𝑑ϕ=aE(ϕ,k=ϵ).\displaystyle s_{BP}=a\int_{0}^{\phi}\sqrt{1-\epsilon^{2}\sin^{2}\phi^{\prime}}\,d\phi^{\prime}=a\,E(\phi,k=\epsilon). (16)

This relation between the arc length of the ellipse and the function E(ϕ,k)E(\phi,k) is the reason why Fagnano (cited in Ref. Prasolov97, ) called FF, EE, and Π\Pi elliptic integrals and provides a direct interpretation of the modulus of the JEFs.

Refer to caption
Figure 2: Representations of points and angles on the ellipse that appear in the definitions and relations involving Jacobi elliptic functions. The figure shows the polar angle θ\theta and the complementary of the eccentricity angle ϕ\phi. The smaller circle of radius bb (dashed line) is inscribed in the ellipse and has common points at ±B=(0,±b,0)\pm B=\left(0,\pm b,0\right). The ellipse is also inscribed in the larger circle with radius aa (dash-dotted line) which has two points in common ±A=(±a,0,0)\pm A=\left(\pm a,0,0\right).

The geometric interpretation of JEFs’ argument uu is less direct and not unique. Fagnano discovered that for k1=2k^{-1}=\sqrt{2}, the elliptic integral of the first kind describes the arc length on the lemniscate defined by the relation r2=cos2θr^{2}=\cos 2\theta (using the same definitions of rr and θ\theta as in Fig. 2).Prasolov97 ; Armitage06 Serret, building on the work of Fagnano and Legendre, found a set of curves on which F(ϕ,k)F(\phi,k) at arbitrary value of k(1,1)k\in(-1,1) is an arc length (see, e.g. Ref. Prasolov97, ). There is also a counterpart in three dimensions: Seiffert’s spirals defined on a sphere. The arc length of the spiral is given by the first elliptic integral.Erdos00 In these examples the argument uu of the JEF is the length of the Serret curve or the Seiffert spiral.

Additional geometric interpretations of the argument uu can be found from trigonometry as it applies to an ellipse using geodesy and elliptic geometry. This is discussed in detail in Refs. Bowman53, and bakerMS12, . All of these interpretations relate uu to a length of some geometric form related to an ellipse. It is important, however, to realize that the angles used to define uu are different for each physical situation. This leads to the important insight that the argument uu has no unique geometric interpretation beyond being an arc length and only has a physical interpretation in some special cases.Bowman53 ; Armitage06 ; bakerMS12

III The Bead on the Hoop

In this section we present an application of Jacobi elliptic functions to a well-known problem. Consider a bead of mass mm that slides without friction on a hoop of radius RR rotating with constant angular velocity ω=ϕ˙\omega=\dot{\phi} (see Fig. 3). In spherical coordinates (r,θ,ϕ)(r,\theta,\phi) the Lagrangian =TV\mathcal{L}=T-V for this system is

(θ,θ˙,t)=12I0(θ˙2+ω2sin2θ)V0(1cosθ),\mathcal{L}\left(\theta,\dot{\theta},t\right)=\frac{1}{2}I_{0}\left(\dot{\theta}^{2}+\omega^{2}\sin^{2}\theta\right)-V_{0}\left(1-\cos\theta\right), (17)

where I0=mR2I_{0}=mR^{2} and V0=mgRV_{0}=mgR. The zero point of the potential energy is located at the bottom of the hoop. The angles θ\theta and ϕ\phi should not be confused with the angles of same name in Sec. II. The polar angle θ\theta is measured from the bottom of the hoop for consistency with the convention usually used in the limiting case of the simple non-linear pendulum.

Refer to caption
Figure 3: Schematic of a bead on a hoop rotating about the vertical zz-axis at a constant azimuthal frequency ω=ϕ˙\omega=\dot{\phi}. The diamond at θ=±θs\theta=\pm\theta_{s} locates the global minimum of the effective potential at the commonly named stationary point, whereas the star at θ=±θe\theta=\pm\theta_{e} locates the so-called ejection point (see text and Fig. 4). The positions of θs\theta_{s} and θe\theta_{e} are obtained using ω=3ωc/2\omega=3\omega_{c}/2. The motion of the bead is described by the polar angle θ(t)\theta(t) measured from the bottom of the hoop.

There are three variables (r,θ,ϕ)(r,\theta,\phi) and two constraints r=Rr=R and ϕ˙=ω\dot{\phi}=\omega, implying that there is only one generalized coordinate, θ\theta. That is, the motion of the bead is described by the time-dependent function θ(t)\theta\left(t\right).

The discussion of the physical content of the following calculations is greatly aided by the introduction of an effective potential VeffV_{\mathrm{eff}}. Since θ\theta is the only degree of freedom, we combine the azimuthal kinetic energy with the gravitational potential energy and rewrite Eq. (17) as (θ,θ˙,t)=Tθ(θ˙)Veff(θ)\mathcal{L}\left(\theta,\dot{\theta},t\right)=T_{\theta}\left(\dot{\theta}\right)-V_{\mathrm{eff}}(\theta), with

Veff(θ)V0\displaystyle\frac{V_{\mathrm{eff}}\left(\theta\right)}{V_{0}} =\displaystyle= 12(ω2ωc2)sin2θ+(1cosθ)\displaystyle-\frac{1}{2}\left(\frac{\omega^{2}}{\omega_{c}^{2}}\right)\sin^{2}\theta+\left(1-\cos\theta\right) (18)

and ωc2=V0/I0=g/R\omega_{c}^{2}=V_{0}/I_{0}=g/R. As shown in Fig. 4, the qualitative shape of the effective potential depends on the azimuthal frequency ω\omega. One distinguishes two regimes: ωωc\omega\leq\omega_{c} when θ¨0\ddot{\theta}\leq 0, and ω>ωc\omega>\omega_{c} when θ¨>0\ddot{\theta}>0. Since θ0=π\theta_{0}=\pi is always a maximum of VeffV_{\mathrm{eff}}, this position is unstable. On the other hand, θ0=0\theta_{0}=0 is a minimum in the first regime but a local maximum in the second regime where two new stable minima appear at ±θs\pm\theta_{s}. For energies near the minima at ±θs\pm\theta_{s} , the bead will oscillate about θs\theta_{s}, remaining exclusively on one side of the hoop. The stable equilibrium point θs\theta_{s} can be obtained by setting the derivative of the effective potential equal to zero. We find

θs(ω)=arccos(ωc2ω2),\theta_{s}(\omega)=\arccos\left(\frac{\omega_{c}^{2}}{\omega^{2}}\right), (19)

which is valid in the supercritical regime (ω>ωc\omega>\omega_{c}).

Refer to caption
Figure 4: (Color online) The effective potential (18) as a function of θ\theta. The dashed line is for ω<ωc\omega<\omega_{c} (for the present plot we chose ω=ωc/5\omega=\omega_{c}/5), the dotted line for ω=ωc\omega=\omega_{c}, and the solid line is for ω>ωc\omega>\omega_{c} (here ω=3ωc/2\omega=3\omega_{c}/2). The diamond at ±θs\pm\theta_{s} and star at ±θe\pm\theta_{e} are indicated in Fig. 3 for the present set of parameters. The effective potential energy at θe\theta_{e} and θ=0\theta=0 is always zero. Note that Veffmax=Veff(π)=2V0V_{\mathrm{eff}}^{\mathrm{max}}=V_{\mathrm{eff}}(\pi)=2V_{0}.

The differential equation governing θ(t)\theta(t) is obtained from the Euler-Lagrange equation associated with Eq. (17)

θ¨=ω22sin2θωc2sinθ,\ddot{\theta}=\frac{\omega^{2}}{2}\sin 2\theta-\omega_{c}^{2}\sin\theta, (20)

and introduce the initial conditions θ(t=0)=θ0\theta(t=0)=\theta_{0} and θ˙(t=0)=θ˙0\dot{\theta}(t=0)=\dot{\theta}_{0}. Without loss of generality, we make use of the symmetry of the problem and define the initial angle θ0\theta_{0} only on one half of the hoop θ0[0,π]\theta_{0}\in\left[0,\pi\right]. Though nonlinear, this differential equation can be solved analytically. The presence of sinθ\sin\theta and sin2θ\sin 2\theta leads to solutions involving JEFs described in Sec. II.

III.1 General Solution of the Euler-Lagrange Equation

We begin by multiplying Eq. (20) by θ˙\dot{\theta} and integrating to obtain

θ˙2(t)ω2+cos2θ(t)2cosθscosθ(t)=𝒞,\frac{\dot{\theta}^{2}(t)}{\omega^{2}}+\cos^{2}\theta(t)-2\cos\theta_{s}\,\cos\theta(t)={\cal C}, (21)

where the constant 𝒞{\cal C} is given by

𝒞cos2θ02cosθscosθ0+(θ˙0ω)2,{\cal C}\equiv\cos^{2}\theta_{0}-2\cos\theta_{s}\cos\theta_{0}+\left(\frac{\dot{\theta}_{0}}{\omega}\right)^{2}, (22)

and θs\theta_{s} is given in Eq. (19). Note that Eq. (21) is not valid for ω=0\omega=0; this situation must be considered separately (see Sec. III.2.3). It is worth mentioning that θs\theta_{s} is nonzero only for ω>ωc\omega>\omega_{c} and takes values in the interval θs[0,π/2]\theta_{s}\in[0,\pi/2]. For ω<ωc\omega<\omega_{c}, only θ0=0\theta_{0}=0 is a stable stationary solution. It is then natural to extend the definition of θs\theta_{s} by imposing θs=0\theta_{s}=0 for the case where ω<ωc\omega<\omega_{c}.

Because 𝒞{\cal C} is a constant, the left hand side of Eq. (21) is a constant of motion of the system. The expression for 𝒞{\cal C} is of particular interest because it allows us to reduce arbitrary initial conditions to ones with zero initial speed. Consider arbitrary initial conditions (θ~0,θ~˙0)(\tilde{\theta}_{0},\dot{\tilde{\theta}}_{0}) for which θ~˙00\dot{\tilde{\theta}}_{0}\neq 0 and Etot<VeffmaxE_{\mathrm{tot}}<V_{\mathrm{eff}}^{\mathrm{max}}. From Eq. (21) we can find a time t0t_{0} and new initial conditions (θ0,θ˙0)(\theta_{0},\dot{\theta}_{0}) with zero initial angular speed θ˙0=0\dot{\theta}_{0}=0 such that θ(t0)=θ~0\theta(t_{0})=\tilde{\theta}_{0} and θ˙(t0)=θ~˙0\dot{\theta}(t_{0})=\dot{\tilde{\theta}}_{0}. The new initial condition (θ0,0)(\theta_{0},0) written in terms of the actual one (θ~0,θ~˙0)(\tilde{\theta}_{0},\dot{\tilde{\theta}}_{0}) is

cosθ0=cosθs±[cosθ~0cosθs]2+1ω2θ~˙02.\cos\theta_{0}=\cos\theta_{s}\pm\sqrt{\left[\cos\tilde{\theta}_{0}-\cos\theta_{s}\right]^{2}+\frac{1}{\omega^{2}}\dot{\tilde{\theta}}_{0}^{2}}. (23)

Thus, arbitrary initial conditions with θ~˙00\dot{\tilde{\theta}}_{0}\neq 0 can be written in terms of initial conditions with θ˙0=0\dot{\theta}_{0}=0. In the following, we limit our discussion to the motion of the bead on the hoop with zero initial speed unless Etot>VeffmaxE_{\mathrm{tot}}>V_{\mathrm{eff}}^{\mathrm{max}}. This case will be discussed later.

We now use the Weierstrass substitutionSpivak06

τ=tan(θ2)=1cosθ1+cosθ,\tau=\tan\left(\frac{\theta}{2}\right)=\sqrt{\frac{1-\cos\theta}{1+\cos\theta}}, (24)

in Eq. (21) and obtain

τ0τ(t)2dτpτ4+2(𝒞+1)τ2+p+=ωt\int_{\tau_{0}}^{\tau\left(t\right)}\frac{2d\tau^{\prime}}{\sqrt{p_{-}\,\tau^{\prime 4}+2\left({\cal C}+1\right)\tau^{\prime 2}+p_{+}}}=\omega t (25)

through separation of variables. This type of equation is usually studied numerically or in limiting cases only.Whittaker37 ; Lima10 ; Bowman53 Here we extend the calculation and invert the integral to obtain θ(t)\theta(t). The structure of the integral implies that the inverse is expressed in terms of JEFs defined in Sec. II.

For convenience, we define τ0=tan(θ0/2)\tau_{0}=\tan\left(\theta_{0}/2\right) and the two constants

p±\displaystyle p_{\pm} \displaystyle\equiv 𝒞1±2cosθs.\displaystyle{\cal C}-1\pm 2\cos\theta_{s}. (26)

After factoring out pp_{-} from the denominator of the integrand in Eq. (25), we write the remaining polynomial under the square root in the form

τ4+2(𝒞+1p)τ2+(p+p)=(τ2γ12)(τ2γ22),\tau^{\prime 4}+2\left(\frac{{\cal C}+1}{p_{-}}\right){\tau^{\prime}}^{2}+\left(\frac{p_{+}}{p_{-}}\right)=\left({\tau^{\prime}}^{2}-\gamma_{1}^{2}\right)\left({\tau^{\prime}}^{2}-\gamma_{2}^{2}\right), (27)

where the roots are given by

γ1,22{a,b}\gamma_{1,2}^{2}\in\left\{a,b\right\} (28)

with

a1cosθ01+cosθ0=τ02,b1+cosθ02cosθs1cosθ0+2cosθs.\displaystyle a\equiv\frac{\textstyle 1-\cos\theta_{0}}{\textstyle 1+\cos\theta_{0}}=\tau_{0}^{2},\quad b\equiv\frac{\textstyle 1+\cos\theta_{0}-2\cos\theta_{s}}{\textstyle 1-\cos\theta_{0}+2\cos\theta_{s}}. (29)

The root aa is always non-negative while bb can take any real value. As a result, the relative values of the two roots aa and bb divides the range θ0[0,π]\theta_{0}\in[0,\pi] into one (for ωωc\omega\leq\omega_{c}) or two (for ω>ωc\omega>\omega_{c}) intervals. When ω>ωc\omega>\omega_{c}, the two intervals are divided by the point b=0b=0, which occurs when the initial condition θ0\theta_{0} takes the value

θe(ω)arccos(2cosθs1)=arccos(2ωc2ω21).\theta_{e}(\omega)\equiv\arccos\left(2\cos\theta_{s}-1\right)=\arccos\left(2\frac{\omega_{c}^{2}}{\omega^{2}}-1\right). (30)

For θ0<θe\theta_{0}<\theta_{e} we have b>0b>0 while for θ0>θe\theta_{0}>\theta_{e} we have b<0b<0. The angle θe\theta_{e} appears in a natural way in our mathematical analysis and is new in the context of the bead and the hoop problem. This angle is represented with a star in Figs. 3 and 4.

We call θe\theta_{e} the “ejection angle” because for any θ0<θe\theta_{0}<\theta_{e}, the bead will remain on the initial half of the hoop forever and never reach the other side. However, when θ0>θe\theta_{0}>\theta_{e} the bead has sufficient energy to cross the relative maximum at θ=0\theta=0 and eject itself from the original half of the hoop where it was released. We note that θe(ωc)=θs(ωc)=0\theta_{e}(\omega_{c})=\theta_{s}(\omega_{c})=0 which compels us to extend their definition by imposing θe=θs=0\theta_{e}=\theta_{s}=0 for ωωc\omega\leq\omega_{c}. The two angles θs\theta_{s} and θe\theta_{e} also satisfy the inequality θeθs\theta_{e}\geq\theta_{s} and θe[0,π]\theta_{e}\in[0,\pi] where θe(ω)π\theta_{e}(\omega\to\infty)\to\pi. Curiously, we observe that Vg(θe)=2Vg(θs)V_{g}\left(\theta_{e}\right)=2V_{g}\left(\theta_{s}\right) but are unaware if this is the result of some physical constraint. Further considerations where the bead is placed directly on this point are addressed in Sec. III.2.1.

The integral Eq. (25), along with Eq. (27), can be related to the first elliptic integral [Eq. (II.1)]. Inversion of the integral gives τ(t)\tau(t) and thus θ(t)\theta(t) using Eq. (24). Which particular inverse JEF equals Eq. (25) depends on γ1\gamma_{1} and γ2\gamma_{2} (or aa and bb).

For ωωc\omega\leq\omega_{c}, we have θs=θe=0\theta_{s}=\theta_{e}=0 and a=b0a=b\geq 0 for θ0[0,π]\theta_{0}\in[0,\pi]. From the tables in Ref. Byrd71, with γ12=a\gamma_{1}^{2}=a and γ22=b\gamma_{2}^{2}=b in Eq. (27), we identify the cosine-amplitude. Transforming back to the variable θ=2arctanτ\theta=2\arctan\tau, we obtain

tan[θ(t)2]=acn[12ωt|p|(a+|b|),aa+|b|].\displaystyle\tan\left[\frac{\theta(t)}{2}\right]=\sqrt{a}\,\mathrm{cn}\left[\frac{1}{2}\omega t\sqrt{\left|p_{-}\right|\left(a+\left|b\right|\right)},\sqrt{\frac{a}{a+\left|b\right|}}\right].\quad (31)

On the other hand, when ω>ωc\omega>\omega_{c} the range θ0[0,π]\theta_{0}\in[0,\pi] is divided into three intervals [0,θs][0,\theta_{s}], [θs,θe][\theta_{s},\theta_{e}], and [θe,π][\theta_{e},\pi], each of which leads to a solution involving a different JEF. For θ0[0,θs]\theta_{0}\in\left[0,\theta_{s}\right] the roots obey the inequality b>a0b>a\geq 0; for θ[θs,θe]\theta\in\left[\theta_{s},\theta_{e}\right] we have a>b0a>b\geq 0; and for θ[θe,π]\theta\in[\theta_{e},\pi] we have a0ba\geq 0\geq b. Using again the table of integrals in Ref. Byrd71, we set γ12=a\gamma_{1}^{2}=a and γ22=b\gamma_{2}^{2}=b for regions θ0(0,θs)\theta_{0}\in\left(0,\theta_{s}\right) and θ0(θe,π)\theta_{0}\in\left(\theta_{e},\pi\right), whereas γ12=b\gamma_{1}^{2}=b and γ22=a\gamma_{2}^{2}=a for θ0(θs,θe)\theta_{0}\in\left(\theta_{s},\theta_{e}\right). This allows identifying the Jacobi elliptic functions nd, dn, and cn, respectively. The third interval θeθπ\theta_{e}\leq\theta\leq\pi, turns out to lead to an expression that is identical to Eq. (31) above.

One can reduce the three cases for ω>ωc\omega>\omega_{c} to one single expression for the entire interval [0,π][0,\pi] by using properties of the JEFs derived in Sec. II.1 and Appendix A. The simplest form of the solution is found in terms of the delta-amplitude function, which naturally appears in the second interval. The cosine-amplitude function appearing in Eq. (31) can be transformed into a delta-amplitude with Eq. (45). Similarly, using the relation discussed after Eq. (46), knd(u,k)=dn(u+K,k)k^{\prime}\,\mathrm{nd}(u,k)=\mathrm{dn}(u+K,k), it is possible to reduce the nd{\rm nd} solution in the first interval to a delta-amplitude function. Careful consideration of the argument (u,k)(u,k) in the transformation leads to the final result

θ(t)\displaystyle\theta\left(t\right) =\displaystyle= 2arctan{adn[12ωt|p|a,aba]},\displaystyle 2\arctan\left\{\sqrt{a}\,\mathrm{dn}\left[\frac{1}{2}\omega t\sqrt{\left|p_{-}\right|\,a},\sqrt{\frac{a-b}{a}}\right]\right\}, (32)
θ0[0,π].\displaystyle\hskip 129.16626pt\theta_{0}\in\left[0,\pi\right].

This is the exact solution of the equation of motion (20), which fully describes the motion of a bead on a spinning hoop for arbitrary initial conditions (θ0,θ˙0)(\theta_{0},\dot{\theta}_{0}), excepting the cases where EtotVg(π)E_{\mathrm{tot}}\geq V_{g}(\pi) or ω=0\omega=0. Equation (32) simplifies to θ(t)=θs\theta(t)=\theta_{s} for all times if θ0=θs\theta_{0}=\theta_{s}. This solution improves or complements previous studies of different variants of the problem.Taylor05 ; Ochoa06 ; Lima10 ; Rousseaux09 ; Bowman53 ; Whittaker37

We note that the argument u(t)u(t) of the JEF is a linear function of time and is proportional to ϕ=ωt\phi=\omega t given by Eq. (25). As pointed out in Sec. II, it is only in special cases that the argument has a useful physical interpretation, and the bead on the hoop is not one of them. In fact, the problem is slightly more difficult than what was presented in the previous section because the JEF was only identified after performing a Weierstrass substitution on the integral of Eq. (25). The Weierstrass substitution can be shown to be a particular mapping of the position of the bead onto the xyxy-plane. The map is obtained from the intersection between the xyxy-plane and the line passing through the top of the hoop and through the bead. The argument u(t)u(t) is related to the arc length (R|p|a/2)ϕ(R\sqrt{|p_{-}|\,a}/2)\,\phi on this stereographic projection.bakerMS12

III.2 Limiting and Special Cases

We discuss the special cases not considered in the previous section: the separatrices (E=0, 2mgRE=0,\,2mgR), the free spinning of the bead around the hoop (E>2mgRE>2mgR), and the general solution for the pendulum (ω=0\omega=0). For all these cases the roots (29) take values a,ba,b\to\infty or 0 and the determination of θ(t)\theta(t) requires special care.

III.2.1 Separatrices

Figure 5 shows phase plots for this problem. The separatrices form the boundaries between qualitatively different motions of the system. They can be understood as delineating a phase change and typically involve functions which are asymptotic to some value. Below, we obtain simple analytical expressions for the separatrices that allow us to plot Fig. 5 without the need of a numerical procedure applied to Eq. (25).

Refer to caption
Refer to caption
Figure 5: (Color online) Phase plots drawn from analytical expressions for (a) subcritical (ωωc\omega\leq\omega_{c}) and (b) supercritical (ω>ωc\omega>\omega_{c}) cases with the values given in Fig. 4. The stars (±θe\pm\theta_{e}) and diamonds (±θs\pm\theta_{s}) indicate the stable dynamical equilibrium points. The solid lines correspond to the periodic motion of the bead inside one of two potential wells. The dashed lines are motions of the bead across the two potential wells. The dotted lines correspond to the spinning of the bead around the hoop. The two thick lines (solid and dashed) are the separatrices.

As seen in Fig. 5b, there are two separatrices when ω>ωc\omega>\omega_{c}. The innermost separatrix (dashed thick line) passing through (θ0,θ˙0)=(0,0)(\theta_{0},\dot{\theta}_{0})=(0,0) separates the cases θ0<θe\theta_{0}<\theta_{e} from θe<θ0<π\theta_{e}<\theta_{0}<\pi. When θ0<θe\theta_{0}<\theta_{e} the periodic motion is limited to either of the two wells of VeffV_{\mathrm{eff}} (see Fig. 4) and the bead oscillates exclusively on the half of the hoop where it started. By contrast, starting positions in the range θe<θ0<π\theta_{e}<\theta_{0}<\pi involve the bead oscillating between the two sides of the hoop and moving through both wells.

The expression θ˙(θ)\dot{\theta}(\theta) of the inner separatrix is obtained from Eq. (21) by noting that θ0=θ˙0=0\theta_{0}=\dot{\theta}_{0}=0 is one point of the separatrix. At that point 𝒞=12cosθs\mathcal{C}=1-2\cos\theta_{s}, which implies that any other point of the separatrix satisfies the equation

θ˙2ω2=(1cosθ)(1+cosθ2cosθs).\dfrac{\dot{\theta}^{2}}{\omega^{2}}=\left(1-\cos\theta\right)\left(1+\cos\theta-2\cos\theta_{s}\right). (33)

The inner separatrix has the shape of a lemniscate as shown by the thick dashed line in Fig. 5b.

The motion on the separatrix is obtained from Eq. (25). The result obtained for arbitrary initial condition on the separatrix is rather involved when (θ0,θ˙0)(θe,0)(\theta_{0},\dot{\theta}_{0})\neq(\theta_{e},0) and will not be needed in the following. For the simpler case of θ0=θe\theta_{0}=\theta_{e}, Eq. (25) or (32) becomes

θ(t)=2arctan[ω2ωc21sech(ωctω2ωc21)],\displaystyle\theta(t)=2\arctan\left[\sqrt{\frac{\omega^{2}}{\omega_{c}^{2}}-1}\,\,\,\mathrm{sech}\left(\omega_{c}\,t\sqrt{\frac{\omega^{2}}{\omega_{c}^{2}}-1}\right)\right],\quad (34)

which is valid for ω>ωc\omega>\omega_{c}. We note that in this case the point (θ,θ˙)=(0,0)(\theta,\dot{\theta})=(0,0) is an unstable equilibrium position. If the bead starts at any other initial condition (for example at θe\theta_{e} and θ˙0=0\dot{\theta}_{0}=0) the bead will need an infinite amount of time to reach the bottom of the hoop.

The second separatrix divides the phase plot between oscillations of the bead that reach both halves of the hoop, and the “free” rotation of the bead around the hoop when Etot>VeffmaxE_{\mathrm{tot}}>V_{\mathrm{eff}}^{\mathrm{max}}. The equation of this separatrix can be obtained from Eq. (21) by noting that (θ0=π,θ˙0=0)(\theta_{0}=\pi,\dot{\theta}_{0}=0) is one point on the separatrix. At that point Eq. (22) reads 𝒞=1+2cosθs{\cal C}=1+2\cos\theta_{s}, which immediately implies from (21) that at any other point of the separatrix we have

θ˙2ω2=(1+cosθ)(1cosθ+2cosθs).\dfrac{\dot{\theta}^{2}}{\omega^{2}}=\left(1+\cos\theta\right)\left(1-\cos\theta+2\cos\theta_{s}\right). (35)

This separatrix is the thick solid line in Figs. 5a and 5b. Any initial condition away from (θ0,θ˙0)=(π,0)(\theta_{0},\dot{\theta}_{0})=(\pi,0) on the separatrix will lead the bead to tend toward π\pi for tt\rightarrow\infty. To obtain θ(t)\theta(t) for initial conditions lying on this second separatrix we integrate Eq. (25) to get

θ(t)\displaystyle\theta\left(t\right) =\displaystyle= 2arctan(cosθs1+cosθssinh{ωt1+cosθs+arcsinh[tan(θ02)1+cosθscosθs]}).\displaystyle 2\arctan\left(\sqrt{\frac{\cos\theta_{s}}{1+\cos\theta_{s}}}\sinh\left\{\omega t\sqrt{1+\cos\theta_{s}}+\mathrm{arcsinh}\left[\tan\left(\frac{\theta_{0}}{2}\right)\,\sqrt{\frac{1+\cos\theta_{s}}{\cos\theta_{s}}}\right]\right\}\right). (36)

The results of this subsection leads to the important observation that the separatrices are not described in terms of JEFs. Instead they depend solely on trigonometric and hyperbolic functions. A further observation is that the time evolution along the separatrices is not periodic but is asymptotic towards an unstable extremum.

III.2.2 Free spinning

For initial derivatives θ˙0\dot{\theta}_{0} greater than the right hand side of Eq. (35), we are outside the second separatrix in the phase plot and the bead is spinning freely on the hoop. Such motion is obtained, for example, when θ0=π\theta_{0}=\pi and θ˙00\dot{\theta}_{0}\neq 0 for which Etot>VeffmaxE_{\mathrm{tot}}>V_{\mathrm{eff}}^{\mathrm{max}}. Any other initial condition (θ0,θ˙00)(\theta_{0},\dot{\theta}_{0}\neq 0) such that the total energy of the bead is larger than VeffmaxV_{\mathrm{eff}}^{\mathrm{max}} can be mapped to this initial condition at θ0=π\theta_{0}=\pi. To obtain the motion θ(t)\theta(t) of the bead in this special case it is, once more, easier to start with Eqs. (21)–(26). For (θ0=π,θ˙00)(\theta_{0}=\pi,\dot{\theta}_{0}\neq 0) we have from Eq. (26) p=θ˙02/ω2p_{-}=\dot{\theta}_{0}^{2}/\omega^{2}, p+=4cosθs+pp_{+}=4\cos\theta_{s}+p_{-} and τ0\tau_{0}\to\infty. The solution is written in terms of the tangent-amplitude function tn=sn/cn\mathrm{tn}=\mathrm{sn}/\mathrm{cn}. The integration of Eq. (27) leads to

θ(t)=2arctan[|γ|tn(12|γθ˙0|t,|γ2||γ+2||γ2|)],\theta\left(t\right)=2\arctan\left[\frac{\left|\gamma_{-}\right|}{\mathrm{tn}\left(-\frac{1}{2}\left|\gamma_{-}\dot{\theta}_{0}\right|\,t,\sqrt{\frac{\left|\gamma_{-}^{2}\right|-\left|\gamma_{+}^{2}\right|}{\left|\gamma_{-}^{2}\right|}}\right)}\right], (37)

but with the roots γ1/2=γ+/\gamma_{1/2}=\gamma_{+/-} given by

γ±2=2[Γ+12]±2Γ2+ω22θ˙0(1cosθs),\displaystyle\gamma_{\pm}^{2}=-2\left[\Gamma+\frac{1}{2}\right]\pm 2\sqrt{\Gamma^{2}+\frac{\omega^{2}}{2\dot{\theta}_{0}}\left(1-\cos\theta_{s}\right)}, (38)

with Γ=(ω2/θ˙02)(1+cosθs)\Gamma=(\omega^{2}/\dot{\theta}_{0}^{2})\left(1+\cos\theta_{s}\right). The oscillation of the bead corresponds to the open dotted lines outside the second separatrix in Fig. 5b (and outside the separatrix of Fig. 5a for ωωc\omega\leq\omega_{c}).

For |θ˙0|\left|\dot{\theta}_{0}\right|\rightarrow\infty, γ±=1\gamma_{\pm}=-1 and Eq. (25) reduces to the form of the arctangent function given in Eq. (1). This implies that as θ˙0\dot{\theta}_{0} increases without bound, our solution approaches the form θ(t)=|θ˙0|t\theta(t)=\left|\dot{\theta}_{0}\right|t. We recognize this as characteristic of a free-particle solution.

III.2.3 General solution for pendulum (ω=0\omega=0)

The pendulum is described by Eq. (20) for ω=0\omega=0 and thus reads θ¨=ωc2sinθ\ddot{\theta}=-\omega_{c}^{2}\,\sin\theta. The solution derived in Sec. III.1 is inapplicable to this case since we divided Eq. (20) by ω\omega to get Eq. (21). We can nevertheless follow a similar path as in Sec. III.1 for this simplified equation of motion. The effective potential (18) with ω=0\omega=0 gives Veff=Vg(θ)V_{\mathrm{eff}}=V_{g}(\theta) and displays a single minimum at θ=0\theta=0 (dashed curve in Fig. 4). The equation for θ˙(t)\dot{\theta}(t) with θ˙0=0\dot{\theta}_{0}=0 corresponding to Eq. (21) is

θ˙(t)2ωc2cosθ(t)=𝒞,\displaystyle\dot{\theta}(t)-2\omega_{c}^{2}\cos\theta(t)={\cal C}, (39)

with 𝒞=θ˙02/2ωc2cosθ0{\cal C}=\dot{\theta}^{2}_{0}/2-\omega_{c}^{2}\cos\theta_{0}. This leads to a phase plot similar to that shown in Fig. 5a. For initial conditions located inside the separatrix there are two possible states of the bead. For θ0=0\theta_{0}=0 we have θ(t)=0\theta(t)=0, the equilibrium position. For θ0(0,π)\theta_{0}\in(0,\pi) and considering first the case θ˙0=0\dot{\theta}_{0}=0 the solution obtained by integrating Eq. (39) (see Sec. III.1) involves a delta-amplitude Jacobi elliptic function

θ(t)=2arctan{γ+dn[ωctcos(θ02)|γ+|,γ+2γ2γ+2]},\displaystyle\theta\left(t\right)=2\arctan\left\{\gamma_{+}\mathrm{dn}\left[\omega_{c}t\cos\left(\frac{\theta_{0}}{2}\right)\left|\gamma_{+}\right|,\sqrt{\dfrac{\gamma_{+}^{2}-\gamma_{-}^{2}}{\gamma_{+}^{2}}}\right]\right\}, (40)

with

γ+2=1cosθ01+cosθ0,γ2=1.\gamma_{+}^{2}=\dfrac{1-\cos\theta_{0}}{1+\cos\theta_{0}},\quad\gamma_{-}^{2}=-1. (41)

This expression is a special case of the general solution (32) and has been discussed in Refs. Whittaker37, ; Lima10, ; Bowman53, .

The separatrix is obtained from Eq. (39) and θ˙0=0\dot{\theta}_{0}=0 with θ0=π\theta_{0}=\pi. Integrating that expression one more time leads to the motion of the bead along the separatrix

θ(t)=2arctan{sinh[ωct+arcsinh(tanθ02)]}.\theta\left(t\right)=2\arctan\left\{\sinh\left[\omega_{c}t+\mathrm{arcsinh}\left(\tan\dfrac{\theta_{0}}{2}\right)\right]\right\}. (42)

Finally, the free spinning case can be obtained in ways similar to the previous sections. We assume (θ0=π,θ˙00)(\theta_{0}=\pi,\dot{\theta}_{0}\neq 0) and obtain Eq. (37) with the new roots (see also Ref. Lima10, )

γ+2=1,γ2=14θ˙02+ωc214θ˙02.\gamma_{+}^{2}=-1,\quad\gamma_{-}^{2}=\dfrac{\tfrac{1}{4}\dot{\theta}_{0}^{2}+\omega_{c}^{2}}{\tfrac{1}{4}\dot{\theta}_{0}^{2}}. (43)

IV Conclusion

We introduced Jacobi elliptic functions using integral inversion and discussed their properties and the meaning of their arguments (u,k)(u,k). The first argument of the JEFs, uu, was shown to be related to an arc length in elliptic geometry, while the second argument kk is the eccentricity. As an application of JEFs, we discussed the motion of the bead on the hoop and derived the complete analytical solution of the problem. Our results reduce to the solution of the pendulum when the hoop rotation frequency vanishes. Interestingly, all motions of the bead on the hoop are written in terms of a Jacobi elliptic function, except for equilibria positions and separatrices, where JEFs reduce to trigonometric and hyperbolic functions or constants. The knowledge of JEFs allows expressing the complete solution of the bead on the hoop problem in an elegant and concise form. These functions and their salient features should be remembered as they may appear in number of other problems in physics.

Acknowledgements.
We gratefully acknowledge the support of the National Science Foundation under grant DMR-0907242, the block grant of CNSM and the graduate research fellowship at CSU Long Beach.

Appendix A Additional properties of Jacobi elliptic functions

We introduced Jacobi elliptic functions in Sec. II and presented their main properties. We summarize in this Appendix a few additional properties of JEFs that were used in solving the bead on the hoop problem.

The JEFs can be related to each other by an appropriate change of variables. For example, starting with the equation u=F(y,k)u=F(y,k), its inversion gives y=sn(u,k)y=\mathrm{sn}(u,k). On the other hand, multiplying both sides of the equation by kk and changing variable t=ktt^{\prime}=k\,t in F(y,k)F(y,k), we can again invert the equation to obtain ky=sn(ku,k1)k\,y=\mathrm{sn}(k\,u,k^{-1}). Thus, we found the first of the following relations

ksn(u,k)=sn(ku,k1),\displaystyle k\,\mathrm{sn}(u,k)=\mathrm{sn}(k\,u,k^{-1}), (44)
dn(u,k)=cn(ku,k1).\displaystyle\mathrm{dn}(u,k)=\mathrm{cn}(k\,u,k^{-1}). (45)

The second relation is obtained from the first, using Eqs. (9) and (10). We use the second equation in Sec. III. Note that in other references, k2=mk^{2}=m is used.

The derivatives of the JEFs with respect to uu can be determined by using their definitions as well. For example, from Eq. (6) one obtains dsnu/du=cnudnud\,\mathrm{sn}u/du=\mathrm{cn}u\,\mathrm{dn}u. From the Taylor expansions of the trigonometric functions one can also expand the JEFs in powers of uu. Addition formulae can be derived from Eqs. (6)–(8). For example,

sn(u+v)\displaystyle\mathrm{sn}(u+v) =\displaystyle= snucnvdnv+snvcnudnuΔ(u,v),\displaystyle\frac{\mathrm{sn}u\,\mathrm{cn}v\,\mathrm{dn}v+\mathrm{sn}v\,\mathrm{cn}u\,\mathrm{dn}u}{\Delta(u,v)}, (46)
dn(u+v)\displaystyle\mathrm{dn}(u+v) =\displaystyle= dnudnvk2snusnvcnucnvΔ(u,v),\displaystyle\frac{\mathrm{dn}u\,\mathrm{dn}v-k^{2}\,\mathrm{sn}u\,\mathrm{sn}v\,\mathrm{cn}u\,\mathrm{cn}v}{\Delta(u,v)}, (47)

with Δ(u,v)=1k2sn2usn2v\Delta(u,v)=1-k^{2}\,\mathrm{sn}^{2}u\,\mathrm{sn}^{2}v. This definition relates to Δ(u)\Delta(u) introduced in the paragraph preceding Eq. (8) via the equality Δ(u)=Δ(u,K)\Delta(u)=\Delta(u,K). These addition formulae allow establishing relations between different JEFs as well. We used one of them in Sec. III.1, namely knd(u,k)=dn(u+K,k)k^{\prime}\,\mathrm{nd}(u,k)=\mathrm{dn}(u+K,k). This relation can be obtained using Eq. (47) with v=Kv=K.

Finally, the JEFs were defined for uu\in\mathbb{R}, but their definition can be extended to the complex plane with the help of the above addition formulae. For example, using Eq. (46) one can decompose sn(x+iy)\mathrm{sn}(x+iy) into real and imaginary parts. In the complex plane, the JEFs are double-periodic functions with periods given by integer multiples of the complete elliptic integral of the first kind.

Further definitions, properties, and expressions can be found in Refs. Bowman53, , Armitage06, ; Neville71, ; Chandrasekharan85, ; bakerMS12, , and Byrd71, .

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