22 Jacobian Elliptic FunctionsApplications22.18 Mathematical Applications22.20 Methods of Computation

- §22.19(i) Classical Dynamics: The Pendulum
- §22.19(ii) Classical Dynamics: The Quartic Oscillator
- §22.19(iii) Nonlinear ODEs and PDEs
- §22.19(iv) Tops
- §22.19(v) Other Applications

With appropriate scalings, Newton’s equation of motion for a pendulum with a mass in a gravitational field constrained to move in a vertical plane at a fixed distance from a fulcrum is

22.19.1 | $$\frac{{\mathrm{d}}^{2}\theta \left(t\right)}{{\mathrm{d}t}^{2}}=-\mathrm{sin}\theta \left(t\right),$$ | ||

$\theta $ being the angular displacement from the point of stable equilibrium, $\theta =0$. The bounded $\left(-\pi \le \theta \le \pi \right)$ oscillatory solution of (22.19.1) is traditionally written

22.19.2 | $$\mathrm{sin}\left(\frac{1}{2}\theta \left(t\right)\right)=\mathrm{sin}\left(\frac{1}{2}\alpha \right)\mathrm{sn}\left(t,\mathrm{sin}\left(\frac{1}{2}\alpha \right)\right),$$ | ||

for an initial angular displacement $\alpha $, with $\mathrm{d}\theta /\mathrm{d}t=0$ at
time $0$; see Lawden (1989, pp. 114–117). The period is
$4K\left(\mathrm{sin}\left(\frac{1}{2}\alpha \right)\right)$. The angle $\alpha =\pi $ is a
*separatrix*,
separating oscillatory and unbounded motion. With the same
initial conditions, if the sign of gravity is reversed then the new period is
$4{K}^{\prime}\left(\mathrm{sin}\left(\frac{1}{2}\alpha \right)\right)$; see Whittaker (1964, §44).

Alternatively, Sala (1989) writes:

22.19.3 | $$\theta \left(t\right)=2\mathrm{am}\left(t,\sqrt{2/E}\right),$$ | ||

for the initial conditions $\theta \left(0\right)=0$, the point of stable equilibrium for
$E=0$, and $\mathrm{d}\theta \left(t\right)/\mathrm{d}t=\sqrt{2E}$. Here
$E=\frac{1}{2}{\left(\mathrm{d}\theta \left(t\right)/\mathrm{d}t\right)}^{2}+1-\mathrm{cos}\theta \left(t\right)$ is the
*energy*, which is a first integral of the motion.
This formulation gives the bounded and unbounded solutions from the same
formula (22.19.3), for $k\ge 1$ and $k\le 1$, respectively.
Also, $\theta \left(t\right)$ is not restricted to the principal range $-\pi \le \theta \le \pi $. Figure 22.19.1 shows the nature of the solutions
$\theta \left(t\right)$ of (22.19.3) by graphing $\mathrm{am}\left(x,k\right)$ for both
$0\le k\le 1$, as in Figure 22.16.1, and $k\ge 1$, where it
is periodic.

Classical motion in one dimension is described by Newton’s equation

22.19.4 | $$\frac{{\mathrm{d}}^{2}x\left(t\right)}{{\mathrm{d}t}^{2}}=-\frac{\mathrm{d}V\left(x\right)}{\mathrm{d}x},$$ | ||

where $V\left(x\right)$ is the potential energy, and $x\left(t\right)$ is the coordinate as a function of time $t$. The potential

22.19.5 | $$V\left(x\right)=\pm \frac{1}{2}{x}^{2}\pm \frac{1}{4}\beta {x}^{4}$$ | ||

plays a prototypal role in classical mechanics (Lawden (1989, §5.2)), quantum mechanics (Schulman (1981, Chapter 29)), and quantum field theory (Pokorski (1987, p. 203), Parisi (1988, §14.6)). Its dynamics for purely imaginary time is connected to the theory of instantons (Itzykson and Zuber (1980, p. 572), Schäfer and Shuryak (1998)), to WKB theory, and to large-order perturbation theory (Bender and Wu (1973), Simon (1982)).

For $\beta $ real and positive, three of the four possible combinations of signs give rise to bounded oscillatory motions. We consider the case of a particle of mass 1, initially held at rest at displacement $a$ from the origin and then released at time $t=0$. The subsequent position as a function of time, $x\left(t\right)$, for the three cases is given with results expressed in terms of $a$ and the dimensionless parameter $\eta =\frac{1}{2}\beta {a}^{2}$.

This is an example of *Duffing’s equation*; see
Ablowitz and Clarkson (1991, pp. 150–152) and
Lawden (1989, pp. 117–119). The subsequent time evolution is always
oscillatory with period $4K\left(k\right)/\sqrt{1+\eta}$:

22.19.6 | $$x\left(t\right)=a\mathrm{cn}\left(\sqrt{1+\eta}t,1/\sqrt{2+{\eta}^{-1}}\right).$$ | ||

There is bounded oscillatory motion near $x=0$, with period $4K\left(k\right)/\sqrt{1-\eta}$, for initial displacements with $\left|a\right|\le \sqrt{1/\beta}$:

22.19.7 | $$x\left(t\right)=a\mathrm{sn}\left(\sqrt{1-\eta}t,1/\sqrt{{\eta}^{-1}-1}\right).$$ | ||

As $a\to \sqrt{1/\beta}$ from below the period diverges since $a=\pm \sqrt{1/\beta}$ are points of unstable equilibrium.

Two types of oscillatory motion are possible. For an initial displacement with $\sqrt{1/\beta}\le \left|a\right|\le \sqrt{2/\beta}$, bounded oscillations take place near one of the two points of stable equilibrium $x=\pm \sqrt{1/\beta}$. Such oscillations, of period $4K\left(k\right)/\sqrt{\eta}$, are given by:

22.19.8 | $$x\left(t\right)=a\mathrm{dn}\left(\sqrt{\eta}t,\sqrt{2-{\eta}^{-1}}\right).$$ | ||

As $a\to \sqrt{2/\beta}$ from below the period diverges since $x=0$ is a point of unstable equlilibrium. For initial displacement with $\left|a\right|\ge \sqrt{2/\beta}$ the motion extends over the full range $-a\le x\le a$:

22.19.9 | $$x\left(t\right)=a\mathrm{cn}\left(\sqrt{2\eta -1}t,1/\sqrt{2-{\eta}^{-1}}\right),$$ | ||

with period $4K\left(k\right)/\sqrt{2\eta -1}$. As $\left|a\right|\to \sqrt{2/\beta}$ from above the period again diverges. Both the $\mathrm{dn}$ and $\mathrm{cn}$ solutions approach $a\mathrm{sech}t$ as $a\to \sqrt{2/\beta}$ from the appropriate directions.

Many nonlinear ordinary and partial differential equations have solutions that may be expressed in terms of Jacobian elliptic functions. These include the time dependent, and time independent, nonlinear Schrödinger equations (NLSE) (Drazin and Johnson (1993, Chapter 2), Ablowitz and Clarkson (1991, pp. 42, 99)), the Korteweg–de Vries (KdV) equation (Kruskal (1974), Li and Olver (2000)), the sine-Gordon equation, and others; see Drazin and Johnson (1993, Chapter 2) for an overview. Such solutions include standing or stationary waves, periodic cnoidal waves, and single and multi-solitons occurring in diverse physical situations such as water waves, optical pulses, quantum fluids, and electrical impulses (Hasegawa (1989), Carr et al. (2000), Kivshar and Luther-Davies (1998), and Boyd (1998, Appendix D2.2)).

The classical rotation of rigid bodies in free space or about a fixed point may
be described in terms of elliptic, or *hyperelliptic*, functions if the
motion is *integrable* (Audin (1999, Chapter 1)). Hyperelliptic
functions
$u\left(z\right)$ are solutions of the equation $z={\int}_{0}^{u}{\left(f\left(x\right)\right)}^{-1/2}\mathrm{d}x$,
where $f\left(x\right)$ is a polynomial of degree higher than 4. Elementary discussions of
this topic appear in Lawden (1989, §5.7),
Greenhill (1959, pp. 101–103), and
Whittaker (1964, Chapter VI). A more abstract overview is
Audin (1999, Chapters III and IV), and a complete discussion of
analytical solutions in the elliptic and hyperelliptic cases appears in
Golubev (1960, Chapters V and VII), the original hyperelliptic
investigation being due to Kowalevski (1889).

Numerous other physical or engineering applications involving Jacobian elliptic functions, and their inverses, to problems of classical dynamics, electrostatics, and hydrodynamics appear in Bowman (1953, Chapters VII and VIII) and Lawden (1989, Chapter 5). Whittaker (1964, Chapter IV) enumerates the complete class of one-body classical mechanical problems that are solvable this way.