Riemannian Geometry of the Contactomorphism Group
Abstract
Given an odddimensional compact manifold and a contact form, we consider the group of contact transformations of the manifold (contactomorphisms) and the subgroup of those transformations that precisely preserve the contact form (quantomorphisms). If the manifold also has a Riemannian metric, we can consider the $L^{2}$ inner product of vector fields on it, which by restriction gives an inner product on the tangent space at the identity of each of the groups that we consider. We then obtain rightinvariant metrics on both the contactomorphism and quantomorphism groups. We show that the contactomorphism group has geodesics at least for short time and that the quantomorphism group is a totally geodesic subgroup of it. Furthermore we show that the geodesics in this smaller group exist globally. Our methodology is to use the right invariance to derive an “Euler–Arnold” equation from the geodesic equation and to show using ODE methods that it has solutions which depend smoothly on the initial conditions. For global existence we then derive a “quasiLipschitz” estimate on the stream function, which leads to a Beale–Kato–Majda criterion which is automatically satisfied for quantomorphisms. Special cases of these Euler–Arnold equations are the Camassa–Holm equation (when the manifold is onedimensional) and the quasigeostrophic equation in geophysics.
Keywords
1 Introduction
The “classical” diffeomorphism groups of a manifold [Banyaga1997] are those groups that preserve a volume form, a symplectic form, a contact form, or a contact structure. A Riemannian metric on the manifold generates a rightinvariant Riemannian metric on the diffeomorphism group, and the geodesic equation of this metric can be written in terms of what is known as the Euler–Arnold equation [Arnold1966, Arnold and Khesin1998] on its Lie algebra. This equation can be expressed as a partial differential equation on the manifold; the bestknown and most important example is the Euler equation of ideal incompressible fluid mechanics, which is the Euler–Arnold equation on the group of volumepreserving diffeomorphisms. The corresponding equation on the group of symplectomorphisms has been studied in [Ebin2012] and [Khesin2012b]; the Euler–Arnold equation in that case coincides with twodimensional hydrodynamics. In this paper we extend these ideas to study the Euler–Arnold equation on the group of contactomorphisms.
Recall that a contact structure on an orientable manifold $M$ of odd dimension $2n+1$ is the nullspace $\mathcal{N}(\theta)$ of some 1form $\theta$ which satisfies the nondegeneracy condition that $\theta\wedge d\theta^{n}$ is nowhere zero. Such a 1form is called a contact form. We will assume that $M$ is equipped with a Riemannian metric which is associated to the contact form [Blair2010] (see Definition 2.2 below), which simplifies our computations, but all of the results are valid regardless of the metric. Let $\mathcal{D}(M)$ be the diffeomorphism group of $M$. Then $\eta\in\mathcal{D}(M)$ is called a contactomorphism if $\eta^{*}\theta$ is a positive multiple of $\theta$, and we denote the group of such contactomorphisms by $\mathcal{D}_{\theta}(M)$. Keeping track of this multiple, we get the group of “padded contactomorphisms” $\widetilde{\mathcal{D}_{\theta}}(M)=\{(\eta,\Lambda)\,\,\eta^{*}\theta=e^{% \Lambda}\theta\}$, a subgroup of the semidirect product $\mathcal{D}(M)\ltimes C^{\infty}(M)$ whose group law is given by
$(\eta,\Lambda)\star(\xi,\Phi)=(\eta\circ\xi,\Lambda\circ\xi+\Phi).$  (1) 
This subgroup will be our main object of interest.
Its Lie algebra may be identified with the space of smooth functions on $M$ (see Proposition 2.1), and the Euler–Arnold equation takes the form
$m_{t}+u(m)+(n+2)mE(f)=0,$  (2) 
where $E$ is the Reeb field (defined below), $u=S_{\theta}f$ is the contact vector field generated by $f$, and $m$ is the momentum given by $m=f\Delta f$ if the Riemannian metric is associated. Equation (2) reduces to the Camassa–Holm equation (3)
$m_{t}+fm_{\alpha}+2mf_{\alpha}=0,\qquad m=ff_{\alpha\alpha},$  (3) 
if $M$ is onedimensional; it is wellknown [Kouranbaeva1999, Misiołek1998] that Eq. (3) is the Euler–Arnold equation on $\mathcal{D}(S^{1})$ with the rightinvariant $H^{1}$ metric. We will see that Eq. (2) has many properties in common with both the Camassa–Holm equation and with twodimensional hydrodynamics.
Our main results are as follows. First we show that (2) can be expressed as a smooth ordinary differential equation on the Hilbert manifold $\widetilde{\mathcal{D}^{s}_{\theta}}(M)$ of padded contactomorphisms of Sobolev class $H^{s}$, when $s>n+3/2$. (Recall that $M$ has dimension $2n+1$.) Therefore we have a smooth Riemannian exponential map which is defined in some neighborhood of zero in $T_{\text{id}}\widetilde{\mathcal{D}^{s}_{\theta}}(M)$. As a consequence we have local wellposedness for (2): for any $f_{0}\in H^{s+1}(M)$ there is a unique solution $f(t)\in H^{s+1}(M)$ defined for $t\in(\varepsilon,\varepsilon)$ of (2) with $f(0)=f_{0}$.
We derive a Beale–Kato–Majda type of global existence criterion for solutions of (2) which says that a solution exists up to time $T$ if and only if the integral
$\int_{0}^{T}\lVert E(f)(t)\rVert_{L^{\infty}}\,dt$ 
is finite. One special case occurs if the metric is associated and the Reeb field $E$ is a Killing field with all orbits closed and of the same length—then we call the metric and contact structure $K$contact and the contact form regular. Under these circumstances solutions of (2) preserve the property that $E(f)=0$ if it is satisfied initially. Such solutions represent geodesics on the group $\mathcal{D}_{q}(M)$ of quantomorphisms, consisting of those diffeomorphisms which preserve the contact form exactly (i.e., $\eta^{*}\theta=\theta$). We show that this is a totally geodesic subgroup for which all geodesics exist globally in time. An alternative view of the quantomorphism group is as a central extension of the group of Hamiltonian diffeomorphisms of the symplectic manifold $N$ which is obtained as a Boothby–Wang quotient of $M$. For this situation the Euler–Arnold equation takes the form $m_{t}+\{f,m\}=0$ with $m=f\Delta f$ on the quotient $N$. This equation is related to the betaplane approximation for the quasigeostrophic equation in geophysical fluid dynamics, as we shall explain.
Finally we discuss two aspects of Eq. (2) which are related to the Camassa–Holm equation. The first is “peakons,” singular solutions of (2) for which the momentum $m$ is initially supported on a set of codimension at least one. The most interesting situation in contact geometry is the case $n=1$ (where $M$ has dimension three) and we consider $m_{0}$ supported on some surface. Then $m(t)$ is supported on a surface $\Gamma(t)$, and we can write an evolution equation for $\Gamma(t)$. This notion has potential application for the study of overtwisted contact structures; see for example [Etnyre et al.2012].
We conclude by proving some conservation laws. It is wellknown that the Camassa–Holm equation is a bihamiltonian equation which is thus completely integrable and has infinitely many conservation laws. The three simplest are $C_{1}=\int_{S^{1}}\sqrt{m_{+}}\,dx$, $C_{0}=\int_{S^{1}}m\,dx$, and $C_{1}=\int_{S^{1}}fm\,d\alpha$, where $m_{+}$ is the positive part of the momentum $m=ff_{\alpha\alpha}$. We show that Eq. (2) has the same three conservation laws, although we do not know if any of the other laws generalize or if there is a bihamiltonian structure.
2 Basic Constructs
2.1 Contact Structures and Contact Forms
A contact manifold $(M,\theta)$ is an orientable manifold $M$ of odd dimension $2n+1$ together with a 1form $\theta$ such that $\theta\wedge d\theta^{n}$ is nowhere zero. The contact structure is a distribution in $TM$ defined at each point $p$ as $\mathcal{N}(\theta)$, the nullspace of $\theta:T_{p}M\rightarrow{\bf R}$. (In the nonorientable case there are contact structures not determined by contact forms, but for simplicity we do not consider these.) In contact geometry one is primarily concerned with the contact structures [Geiges2006, Etnyre et al.2012], and thus a contact form $\theta$ is equivalent to $F\theta$ whenever $F$ is a positive function on $M$. A diffeomorphism $\eta\in\mathcal{D}(M)$ is called a contactomorphism if $\eta^{*}\theta=e^{\Lambda}\theta$ for some function $\Lambda\colon M\to\mathbb{R}$. In some cases one is concerned with the contact form itself, and we say that a quantomorphism is a diffeomorphism $\eta$ such that $\eta^{*}\theta=\theta$; see [Ratiu and Schmid1981] and Sect. 4.1 below for details. The Riemannian geometry of the group of quantomorphisms was studied by [Smolentsev1994], but to our knowledge the Riemannian geometry of the group of contactomorphisms has never been studied in depth.
Our primary concern is with the Lie algebra of contact vector fields, those for which the local flow preserves the contact structure. We review some of the basic concepts; see [Geiges2006] for more details. Given a contact form $\theta$, there is a unique vector field $E$, called the Reeb field, defined by the conditions
$\iota_{E}d\theta=0\quad\text{and}\quad\theta(E)\equiv 1.$ 
The uniqueness of $E$ is a direct consequence of the fact that $\theta\wedge d\theta^{n}$ is never zero. The following characterization of contact vector fields is wellknown.
Proposition 2.1.
The Lie algebra $T_{\text{id}}\mathcal{D}_{\theta}(M)$ consists of vector fields $u$ such that $\mathcal{L}_{u}\theta=\lambda\theta$ for some function $\lambda\colon M\to\mathbb{R}$. Any such field $u$ is uniquely determined by the function $f=\theta(u)$, so we write $u=S_{\theta}f$. In this case the multiplier $\lambda$ is given by $E(f)$. The padded contactomorphism group $\widetilde{\mathcal{D}_{\theta}}(M)$ has Lie algebra of the form
$T_{\text{id}}\widetilde{\mathcal{D}_{\theta}}(M)=\{\widetilde{S_{\theta}}f=(S_% {\theta}f,Ef)\,\,f\in C^{\infty}(M)\}.$ 
Proof.
Given a family of contactomorphisms $\eta(t)$ satisfying $\eta(t)^{*}\theta=e^{\Lambda(t)}\theta$ with $\eta(0)=\text{id}$ and $\dot{\eta}(0)=u$, differentiating at $t=0$ gives $\mathcal{L}_{u}\theta=\dot{\Lambda}(0)\theta$; conversely given any vector field $u$ such that $\mathcal{L}_{u}\theta=\lambda\theta,$ then $\eta(t)$, the flow of $u$, satisfies $\eta(t)^{*}\theta=e^{t\lambda}\theta$. Hence $u\in T_{\text{id}}\mathcal{D}_{\theta}(M)$ iff $\mathcal{L}_{u}\theta=\lambda\theta$ for some function $\lambda$.
Since the Reeb field $E$ is not in the nullspace $\mathcal{N}(\theta)$, any vector field $u$ can be decomposed as $u=v+fE$ where $v\in\mathcal{N}(\theta).$ If $u\in T_{\text{id}}\mathcal{D}_{\theta}(M)$ is decomposed as above, then $f=\theta(u)$, and by the Cartan formula we have $\iota_{u}d\theta+df=\lambda\theta$. Applying both sides to the Reeb field $E$ we obtain $\lambda=E(f)$. The fact that $\theta\wedge d\theta^{n}$ is never zero implies that $d\theta$ must have rank $2n$ at each point. Hence the map $u\mapsto\iota_{u}d\theta$ is an isomorphism in each tangent space $T_{p}M$ from $\mathcal{N}(\theta)\subset T_{p}M$ to $\mathcal{A}(E)\subset T_{p}^{*}M$ (the annihilator of $E$). We denote this map by $\gamma$ and its inverse by $\Gamma$; then $\mathcal{L}_{u}\theta=\lambda\theta$ if and only if $\lambda=E(f)$ and $u=\Gamma(E(f)\thetadf)+fE$, where $f=\theta(u)$. Define $S_{\theta}(f)$ to be $u$. $\square$
By the Darboux theorem [Geiges2006], every contact form can be expressed in some local coordinates $(x^{1},\ldots,x^{n},y^{1},\ldots,y^{n},z)$ as $\theta=dz\sum_{k=1}^{n}y^{k}\,dx^{k}$. In such coordinates the Reeb field is given by $E=\frac{\partial}{\partial z}$, and the operator $S_{\theta}f$ is given in terms of the frame $P_{k}=\frac{\partial}{\partial x^{k}}+y^{k}\,\frac{\partial}{\partial z},$ $Q_{k}=\frac{\partial}{\partial y^{k}}$ and $E$ as
$S_{\theta}f=\sum_{k}Q_{k}(f)P_{k}+\sum_{k}P_{k}(f)Q_{k}+fE.$  (4) 
We note that $S_{\theta}f$ differentiates $f$ in only $2n$ directions, the omitted direction being $E$. This will be important later when we discuss smoothness in the Sobolev context.
The padded contactomorphism group $\widetilde{\mathcal{D}_{\theta}}(M)=\{(\eta,\Lambda)\,\,\eta^{*}\theta=e^{% \Lambda}\theta\}$ has the structure of a semidirect product, since if $\eta^{*}\theta=e^{\Lambda}\theta$ and $\xi^{*}\theta=e^{\Phi}\theta$, then $(\eta\circ\xi)^{*}\theta=\xi^{*}(e^{\Lambda}\theta)=e^{\Lambda\circ\xi+\Phi}\theta$. Hence the group law is as given by ( 1). The Lie bracket is given by
$[\widetilde{S_{\theta}}f,\widetilde{S_{\theta}}g]=\widetilde{S_{\theta}}\{f,g% \},\quad\text{where }\,\,\,\{f,g\}=S_{\theta}f(g)gE(f);$  (5) 
we will refer to this bracket on functions as a “contact Poisson bracket.” Note that unlike a symplectic bracket it does not satisfy the Leibniz rule.
2.2 Associated Riemannian Metrics
We now want to consider a Riemannian structure on $M$. Although in principle the analysis is very similar whether or not the Riemannian metric is related to the contact form in any way, it is convenient to require some stronger compatibility. A reasonable minimum condition is that the volume form generated by the Riemannian metric be a constant multiple of $\theta\wedge(d\theta)^{n}$, which ensures that the Reeb field $E$ is divergencefree. A stronger condition is that the Riemannian metric be associated to the contact form.
Definition 2.2.
If $M$ is a contact manifold with contact form $\theta$ and Reeb field $E$, a Riemannian metric $\langle\cdot,\cdot\rangle$ is called associated if it satisfies the following conditions:

•
$\theta(u)=\langle u,E\rangle$ for all $u\in TM$, and

•
there exists a $(1,1)$tensor field $\phi$ such that $\phi^{2}(u)=u+\theta(u)E$ and $d\theta(u,v)=\langle u,\phi v\rangle$ for all $u$ and $v$.
It is known that every contact manifold has an infinitedimensional family of associated Riemannian metrics [Blair2010].
Having an associated metric allows us to simplify some formulas, as follows.
Proposition 2.3.
Suppose $M$ has a contact form $\theta$ and an associated Riemannian metric as in Definition 2.2. Then we have the following:

•
$E$ is a unit vector field.

•
Contact vector fields are given by
$S_{\theta}f=fE\phi\nabla f$ (6) 
•
The momentum $m=\widetilde{S_{\theta}^{\star}}\widetilde{S_{\theta}}f$ , where $\widetilde{S_{\theta}^{\star}}$ is the formal adjoint of $\widetilde{S_{\theta}}$ , is given by
$m=f\Delta f.$ (7) 
•
There is an orthonormal frame $\{E,P_{1},\ldots,P_{n},Q_{1},\ldots,Q_{n}\}$ such that $\phi(P_{k})=Q_{k}$ , $\phi(Q_{k})=P_{k}$ , and $\phi(E)=0$ . Thus we have $S_{\theta}f=fE+\sum_{k=1}^{n}P_{k}(f)Q_{k}Q_{k}(f)P_{k}$ , as in ( (4) ).

•
If $n\geq 1$ , the Riemannian volume form $\mu$ is given by $\mu=\frac{1}{n}\theta\wedge(d\theta)^{n}$ .

•
For any function $f$ , we have
$\operatorname{div}{(S_{\theta}f)}=(n+1)E(f).$ (8) In particular since $E=S_{\theta}(1)$ , the Reeb field $E$ is divergencefree.
Proof.
$E$ is unit since $\lvert E\rvert^{2}=\theta(E)=1$. Since $\theta(\phi(v))=\langle E,\phi(v)\rangle=d\theta(E,v)=0$ for any vector $v$, we see that $\phi$ maps into the nullspace of $\theta$. Hence if $u=fE\phi\nabla f$ we will have (for any vector field $v$)
$\displaystyle\mathcal{L}_{u}\theta(v)$  $\displaystyle=d\theta(u,v)+v(\theta(u))$  
$\displaystyle=d\theta(fE\phi\nabla f,v)+v(f)$  
$\displaystyle=d\theta(v,\phi\nabla f)+v(f)$  
$\displaystyle=\langle v,\phi^{2}\nabla f\rangle+\langle v,\nabla f\rangle$  
$\displaystyle=\langle v,\nabla f\rangle+\langle v,\theta(\nabla f)E\rangle+% \langle v,\nabla f\rangle$  
$\displaystyle=E(f)\theta(v).$ 
Since this is true for any $v$ we must have $\mathcal{L}_{u}\theta=E(f)\theta$ which means that $u=S_{\theta}f$.
To obtain the formula for the momentum, we need to compute the formal adjoint of $\widetilde{S_{\theta}}.$ Integrating by parts we get:
$\displaystyle\langle\!\langle\widetilde{S_{\theta}}f,\widetilde{S_{\theta}}g% \rangle\!\rangle$  $\displaystyle=\int_{M}\langle S_{\theta}f,S_{\theta}g\rangle\,d\mu+\int_{M}E(f% )E(g)\,d\mu$  
$\displaystyle=\int_{M}(fg+\langle\phi\nabla f,\phi\nabla g\rangle+E(f)E(g))\ d\mu,$ 
since $E$ is orthogonal to the image of $\phi$. Now
$\begin{aligned}\langle\phi\nabla f,\phi\nabla g\rangle=&d\theta(\phi\nabla f,\nabla g)=d \theta(\nabla g,\phi\nabla f)=\langle\nabla g,\phi^{2}\nabla f\rangle\\ =&\langle\nabla g,\nabla f\rangle\langle\nabla g,\theta(\nabla f)E\rangle= \langle\nabla g,\nabla f\rangleE(f)E(g).\end{aligned}$ 
We conclude that
$\displaystyle\int_{M}g\widetilde{S_{\theta}^{\star}}\widetilde{S_{\theta}}f\,d\mu$  $\displaystyle=\langle\!\langle\widetilde{S_{\theta}}f,\widetilde{S_{\theta}}g% \rangle\!\rangle=\int_{M}\big(fg+\langle\nabla f,\nabla g\rangle\big)\,d\mu$  
$\displaystyle=\int_{M}g(f\Delta f)\,d\mu$ 
for any function $g$, as desired.
The orthonormal basis is constructed as follows: take an arbitrary unit vector field $Q_{1}$ orthogonal to $E$, and define $P_{1}=\phi(Q_{1})$; then $\langle P_{1},Q_{1}\rangle=\langle Q_{1},\phi(Q_{1})\rangle=d\theta(Q_{1},Q_{1% })=0$, and $P_{1}$ is orthogonal to $E$ since it is in the image of $\phi$. Clearly $\phi(P_{1})=Q_{1}$. Choose $Q_{2}$ orthogonal to all three, and $P_{2}=\phi(Q_{2})$; then $\langle P_{2},Q_{1}\rangle=\langle\phi Q_{2},Q_{1}\rangle=\langle Q_{2},P_{1}% \rangle=0$ and $\langle P_{2},P_{1}\rangle=\langle\phi Q_{2},\phi Q_{1}\rangle=\langle Q_{2},% Q_{1}\rangle=0$ since $\phi^{2}$ is the negative identity on the orthogonal complement of $E$. We continue in this way to obtain the orthonormal frame, then use the fact that $\nabla f=E(f)E+\sum_{k}P_{k}(f)P_{k}+Q_{k}(f)Q_{k}$ to obtain the formula for $S_{\theta}f$ in the basis.
To compute the Riemannian volume form $\mu$, we note that since the basis is orthonormal, we have $\mu(E,P_{1},\ldots,P_{n},Q_{1},\ldots,Q_{n})=\pm 1$. Now let $\nu=\theta\wedge(d\theta)^{n}$; then we need to compute $\nu(E,P_{1},\ldots,P_{n},Q_{1},\ldots,Q_{n})$. Since $\theta(E)=1$ and $\theta(P_{k})=\theta(Q_{k})=0$, we have
$\nu(E,P_{1},\ldots,P_{n},Q_{1},\ldots,Q_{n})=(d\theta)^{n}(P_{1},\ldots,P_{n},% Q_{1},\ldots,Q_{n}).$ 
In addition we have $d\theta(P_{k},Q_{k})=\langle P_{k},\phi Q_{k}\rangle=1$ for each $k$, so that
$(d\theta)^{n}(P_{1},\ldots,P_{n},Q_{1},\ldots,Q_{n})=nd\theta(P_{1},Q_{1})% \cdots d\theta(P_{n},Q_{n})=n.$ 
Hence $\nu=n\mu$.
Finally to obtain the divergence of $u=S_{\theta}f$, we note that $\mathcal{L}_{u}\theta=E(f)\theta$; hence we have $\mathcal{L}_{u}d\theta=d(E(f)\theta)=dE(f)\wedge\theta+E(f)\,d\theta$. By the product rule for Lie derivatives we obtain $\mathcal{L}_{u}(\theta\wedge d\theta)=2E(f)\theta\wedge d\theta$, and inductively we get $\mathcal{L}_{u}\nu=(n+1)E(u)\nu$. In particular since $E=S_{\theta}(1)$ and $E(1)=0$, the Reeb field is divergencefree. $\square$
Here are some examples of manifolds with associated metrics.
Example 2.4.

•
On $S^{1}$ with coordinate $\alpha$ and the basic 1form $\theta=d\alpha$, we have $E=\frac{\partial}{\partial\alpha}$ and $S_{\theta}f=fE$ with $\widetilde{\Delta_{\theta}}f=ff_{\alpha\alpha}$. The group of contactomorphisms is of course all of $\mathcal{D}(S^{1})$.

•
On any threedimensional unimodular Lie group [Milnor1976] with a frame of leftinvariant vector fields $\{e_{1},e_{2},e_{3}\}$ satisfying $[e_{2},e_{3}]=e_{1}$, denote the dual frame by $\{e_{1}^{\flat},e_{2}^{\flat},e_{3}^{\flat}\}$ and let $\alpha=e_{1}^{\flat}.$ Then the 1form $\alpha$ is a contact form since $\alpha\wedge d\alpha(e_{1},e_{2},e_{3})=\alpha(e_{1})\alpha([e_{2},e_{3}])=1$. Declaring these fields to be orthonormal, we get an associated metric where $S_{\theta}f=fe_{1}e_{3}(f)e_{2}+e_{2}(f)e_{3}$ and $\widetilde{\Delta_{\theta}}=1e_{1}^{2}e_{2}^{2}e_{3}^{2}$. The 3sphere and the Heisenberg group are special cases; in particular on the Heisenberg group the Darboux contact form $dzy\,dx$ has associated metric $ds^{2}=(dzy\,dx)^{2}+dx^{2}+dy^{2}$.

•
On $\mathbb{T}^{3}$ the 1form $\theta=\sin{z}\,dx+\cos{z}\,dy$ is a contact form with the usual flat metric associated, such that $S_{\theta}f=(f\sin{z}+f_{z}\cos{z})\,\partial_{x}+(f\cos{z}f_{z}\sin{z})\,% \partial_{y}+(f_{x}\cos{z}+f_{y}\sin{z})\,\partial_{z}$ and $\widetilde{\Delta_{\theta}}=1\partial_{x}^{2}\partial_{y}^{2}\partial_{z}^{2}$.
2.3 The Riemannian Structure of the Contactomorphism Group
As is usual when studying diffeomorphism groups [Ebin and Marsden1970, Misiołek and Preston2010], the Fréchet manifold structure leads to analytical difficulties when studying geometry due to the lack of an Inverse Function Theorem and to the possibility of nonintegrability of vector fields. Hence we enlarge the group to the set of diffeomorphisms $\eta\in\mathcal{D}^{s}(M)$ of Sobolev class $H^{s}$ for $s>\dim{M}/2+1=n+3/2$, consisting of those maps whose derivatives up to order $s$ are squareintegrable in every coordinate chart of compact support. The index $s$ is large enough to ensure by the Sobolev embedding theorem that $\eta$ and $\eta^{1}$ are both $C^{1}$. We denote by $\mathcal{D}^{s}_{\theta}(M)$ the group of Sobolev $H^{s}$ diffeomorphisms preserving the contact structure; although this is a subgroup of $\mathcal{D}^{s}(M)$, it is not a smooth submanifold since $T_{\text{id}}\mathcal{D}^{s}_{\theta}(M)$ is not a closed subspace of $T_{\text{id}}\mathcal{D}^{s}(M)$. See [Omori1974, Smolentsev2007]. The problem is that $S_{\theta}f$ (as given in coordinates by (4)) does not differentiate the function $f$ in all directions: the derivative in the Reeb direction is missing.
Following [Omori1974], we resolve this by instead considering $\widetilde{\mathcal{D}^{s}_{\theta}}(M)=\{(\eta,\Lambda)\in\mathcal{D}^{s}(M)% \ltimes H^{s}(M)\,\,\eta^{*}\theta=e^{\Lambda}\theta\}$ as a subgroup of $\widetilde{\mathcal{D}^{s}}(M)=\mathcal{D}^{s}(M)\ltimes H^{s}(M)$. Note that requiring $\Lambda\in H^{s}(M)$ is not the obvious definition: $\Lambda$ has more smoothness than would be expected automatically since $\eta^{*}\theta$ is usually only $H^{s1}$ if $\eta\in\mathcal{D}^{s}(M)$. However it is easy to check that for any $f\in H^{s+1}(M)$, the flow $(\eta(t),\Lambda(t))$ of the vector field $\widetilde{S_{\theta}}f$ on $M\times\mathbb{R}$ will satisfy $(\eta(t),\Lambda(t))\in\widetilde{\mathcal{D}^{s}_{\theta}}(M)$ for all $t$. Omori shows (in our notation) that the map $\Psi\colon\widetilde{\mathcal{D}}^{s}(M)\to H^{s1}(\Omega^{1})\oplus H^{s1}(% \Omega^{2})$ defined by
$\Psi(\eta,\lambda)=(e^{\Lambda}\eta^{*}\theta,e^{\Lambda}(d\Lambda\wedge% \eta^{*}\theta+\eta^{*}d\theta))$ 
is smooth and that $\widetilde{\mathcal{D}^{s}_{\theta}}(M)$ is the inverse image of the regular value $(\theta,d\theta)$, so that it is a smooth submanifold. Because of this, we will work primarily with the padded contactomorphism group, so that our geodesic equation ends up being a smooth ordinary differential equation on a Hilbert manifold.
Another approach to the contactomorphism group appears in [Bland and Duchamp2014]; they use the [Folland and Stein1974] topology rather than the usual Sobolev topology, and in this topology the contactomorphism group is a smooth Hilbert submanifold of the diffeomorphism group. The main reason we prefer the present approach is that our geodesic equation ends up having the momentum $m$ in (2) defined in terms of an elliptic operator rather than a subelliptic operator, and the onedimensional equation reduces to the Camassa–Holm equation (3) which is a smooth ODE rather than $u_{t}+3uu_{x}=0$ which is not a smooth ODE [Constantin and Kolev2002].
Given a rightinvariant Riemannian metric on any Lie group $G$, the geodesic equation for a curve $\eta\colon(a,b)\to G$ may be written generally as
$\frac{d\eta}{dt}=dR_{\eta(t)}u(t),\qquad\frac{du}{dt}+\operatorname{ad}_{u}^{*% }u=0$  (9) 
where the second equation is called the Euler–Arnold equation. See for example [Khesin et al.2013] for a survey of such equations. The most famous examples are the Euler equations for an ideal fluid if $G$ is the group of volumepreserving diffeomorphisms, and the Korteweg–deVries and Camassa–Holm equations when $G$ is $\mathcal{D}(S^{1})$ or its central extension. In our case, the simplest rightinvariant Riemannian metric on the semidirect product $\widetilde{\mathcal{D}}(M)$ is given at the identity by
$\langle\!\langle(u,\lambda),(v,\rho)\rangle\!\rangle=\int_{M}\langle u,v% \rangle\,d\mu+\int_{M}\lambda\rho\,d\mu.$  (10) 
The Euler–Arnold equation on a semidirect product has been studied in [Holm et al.1998] and [Vizman2001] in general, and in special cases such as the “twocomponent generalizations” of some wellknown onedimensional Euler–Arnold equations; see for example [Lenells and Wunsch2013] and references therein.
The metric ((10)) induces a rightinvariant metric on the submanifold $\widetilde{\mathcal{D}_{\theta}}(M)$ which at the identity takes the form
$\langle\!\langle\widetilde{S_{\theta}}f,\widetilde{S_{\theta}}g\rangle\!% \rangle=\int_{M}\langle S_{\theta}f,S_{\theta}g\rangle\,d\mu+\int_{M}E(f)E(g)% \,d\mu=\int_{M}(f\Delta f)g\,d\mu,\\ $ 
as computed in Proposition 2.3 for an associated metric. This metric of course gives the same topology as the Sobolev $H^{1}$ metric on functions. More generally (if the Riemannian metric is not associated), the metric (2.3) becomes
$\langle\!\langle\widetilde{S_{\theta}}f,\widetilde{S_{\theta}}g\rangle\!% \rangle=\int_{M}mg\,d\mu,$ 
where $m=\widetilde{S_{\theta}^{\star}}\widetilde{S_{\theta}}f$ is the contact Laplacian (a positivedefinite elliptic operator), and the metric induced on functions is topologically equivalent to the Sobolev $H^{1}$ metric.
We now compute the Euler–Arnold equation on the contactomorphism group.
Proposition 2.5.
Suppose $M$ is a contact manifold with an associated Riemannian metric. Then the Euler–Arnold equation ((9)) on $\widetilde{\mathcal{D}_{\theta}}(M)$ with rightinvariant metric (2.3) is given by (2), where $m=\widetilde{\Delta_{\theta}}f=f\Delta f$.
Proof.
We just need to compute $\operatorname{ad}_{\tilde{u}}^{*}\tilde{u}$, where $\tilde{u}=\widetilde{S_{\theta}}f$ for some stream function $f$. Let $\tilde{v}=\widetilde{S_{\theta}}g$; then we have
$\begin{align}&\langle\!\langle\operatorname{ad}_{\tilde{u}}^{*}\tilde{u},\tilde{v}\rangle \!\rangle=\langle\!\langle\tilde{u},\operatorname{ad}_{\tilde{u}}\tilde{v} \rangle\!\rangle=\langle\!\langle\widetilde{S_{\theta}}f,\widetilde{S_{\theta }}\{f,g\}\rangle\!\rangle=\int_{M}\{f,g\}\widetilde{\Delta_{\theta}}f\,d\mu\\ &\quad=\int_{M}[S_{\theta}f(g)gE(f)]m\,d\mu=\int_{M}g[\operatorname{div}{( mS_{\theta}f)}+mE(f)]\,d\mu,\end{align}$ 
using the formula ((5)) and the fact that the Lie algebra adjoint is the negative of the usual Lie bracket of vector fields.
By Proposition 2.3 we have $\operatorname{div}{(S_{\theta}f)}=(n+1)E(f)$. Hence we have
$\langle\!\langle\operatorname{ad}_{\tilde{u}}^{*}\tilde{u},\tilde{v}\rangle\!% \rangle=\int_{M}g\big(S_{\theta}f(m)+(n+2)mE(f)\big)\,d\mu,$ 
where $m=\widetilde{\Delta_{\theta}}f$. We obtain $\operatorname{ad}_{\tilde{u}}^{*}\tilde{u}=\widetilde{S_{\theta}}{(\widetilde{% \Delta_{\theta}})}^{{}_{1}}[S_{\theta}f(m)+(n+2)mE(f)]$, and applying $\widetilde{S_{\theta}^{\star}}$ to the second equation of ((9)), we obtain (2). $\square$
Every Euler–Arnold equation on a group $G$ has a conservation law (which reflects the symmetry obtained by the Noether theorem, [Abraham et al.1988] resulting from rightinvariance of the metric). In general this comes from rewriting ((9)) as $\frac{d}{dt}\operatorname{Ad}_{\eta(t)}^{*}u(t)=0$ to obtain
$u(t)=\operatorname{Ad}_{\eta(t)^{1}}^{*}u_{0}.$  (11) 
This with the flow equation leads to a firstorder equation on the group $G$ given by
$\frac{d\eta}{dt}=dR_{\eta(t)}\operatorname{Ad}_{\eta(t)^{1}}^{*}u_{0},\qquad% \eta(0)=\text{id},$  (12) 
where $u_{0}\in T_{e}G$ is the initial velocity. For ideal fluid mechanics, Eq. (11) expresses conservation of vorticity; for the Camassa–Holm equation (3) it expresses the conservation of the momentum $m=ff_{\alpha\alpha}$ in the form
$m(t,\eta(t,\alpha))=m_{0}(\alpha)/\eta_{\alpha}(t,\alpha)^{2},$  (13) 
where $m_{0}\colon S^{1}\to\mathbb{R}$ is the initial momentum and $\eta(t)\in\mathcal{D}(S^{1})$ is the Lagrangian flow. In particular if $m_{0}$ is of one sign, then $m(t)$ is always of the same sign. A wellknown result due to [McKean1998] is that the Camassa–Holm equation on the circle has global solutions if and only if the momentum never changes sign; if it does change sign, solutions $u$ blow up in finite time due to $\eta$’s ceasing to be a diffeomorphism. The following lemma relating the Jacobian determinant of $\eta$ to the scaling factor $\Lambda$ will be useful.
Lemma 2.6.
Suppose the Riemannian volume form $\mu$ is a constant multiple of the contact volume form $\nu=\theta\wedge(d\theta)^{n}$, as for example happens when the Riemannian metric is associated (Proposition 2.3). Then whenever $\eta^{*}\theta=e^{\Lambda}\theta$, the Jacobian determinant $\operatorname{Jac}(\eta)$ defined by $\eta^{*}\mu=\operatorname{Jac}(\eta)\mu$ will satisfy
$\operatorname{Jac}(\eta)=e^{(n+1)\Lambda}.$  (14) 
Proof.
Since $\eta^{*}\theta=e^{\Lambda}\theta$, we have $\eta^{*}(d\theta)=d(\eta^{*}\theta)=e^{\Lambda}(d\theta+d\Lambda\wedge\theta)$. Now we have
$\eta^{*}(\theta\wedge d\theta)=(\eta^{*}\theta)\wedge(\eta^{*}d\theta)=e^{2% \Lambda}(\theta\wedge d\theta\theta\wedge\theta\wedge d\Lambda)=e^{2\Lambda}% \theta\wedge d\theta.$ 
Inductively we obtain $\eta^{*}\nu=e^{(n+1)\Lambda}\nu$, and since $\mu$ is a constant multiple of $\nu$ we have $\operatorname{Jac}(\eta)=e^{(n+1)\Lambda}$. Alternatively this is a consequence of the divergence formula (8). $\square$
Now we generalize the conservation law (13) to the higherdimensional situation.
Proposition 2.7.
Let $M$ be a contact manifold of dimension $2n+1$ with an associated Riemannian metric as in Definition 2.2. Then Eq. (2) satisfies the conservation law
$m(t,\eta(t,p))=m_{0}(p)/\operatorname{Jac}(\eta(t,p))^{(n+2)/(n+1)},$  (15) 
where $\eta$ is the Lagrangian flow of $u=S_{\theta}f$ and $\operatorname{Jac}(\eta)$ denotes its Jacobian determinant.
Proof.
For any $(\eta,\Lambda)\in\widetilde{\mathcal{D}_{\theta}}(M)$ and $(v,\phi)\in T_{\text{id}}\widetilde{\mathcal{D}_{\theta}}(M)$, we have by definition that $\operatorname{Ad}_{(\eta,\Lambda)}(v,\phi)=\frac{d}{dt}\big_{t=0}(\eta,% \Lambda)\star(\xi(t),\Phi(t))\star(\eta,\Lambda)^{1}$, where $(\xi(t),\Phi(t))$ is any curve satisfying $\frac{d}{dt}\big_{t=0}(\xi(t),\Phi(t))=(v,\phi)$. From the formula (1) for the group law, it is easy to compute that
$\operatorname{Ad}_{(\eta,\Lambda)}(v,\phi)=(\operatorname{Ad}_{\eta}v,v(% \Lambda)\circ\eta^{1}+\phi\circ\eta^{1}),$ 
where $\operatorname{Ad}_{\eta}v$ is the usual adjoint operator on the diffeomorphism group. We now need to compute what this is when $\eta$ is a contactomorphism and $v=S_{\theta}g$ is a contact vector field. Since $\operatorname{Ad}_{\eta}v$ will also be a contact vector field, we must have $\operatorname{Ad}_{\eta}S_{\theta}g=S_{\theta}h$ where $h=\theta(\operatorname{Ad}_{\eta}v)$. Using $\eta^{*}\theta=e^{\Lambda}\theta$ and the formula $\operatorname{Ad}_{\eta}v=\eta_{*}v\circ\eta^{1}$, it is easy to verify that $h=(e^{\Lambda}g)\circ\eta^{1}$.
We thus compute
$\displaystyle\langle\!\langle\operatorname{Ad}_{(\eta,\Lambda)}^{*}(u,\lambda)% ,(v,\phi)\rangle\!\rangle$  $\displaystyle=\langle\!\langle\widetilde{S_{\theta}}f,\widetilde{S_{\theta}}(e% ^{\Lambda\circ\eta^{1}}(g\circ\eta^{1}))\rangle\!\rangle$  
$\displaystyle=\int_{M}(\widetilde{\Delta_{\theta}}f)e^{\Lambda}g\circ\eta^{1}% \,d\mu$  
$\displaystyle=\int_{M}(\widetilde{\Delta_{\theta}}f\circ\eta)e^{(n+2)\Lambda}g% \,d\mu,$ 
using the change of variables formula and Lemma 2.6. We conclude that
$\operatorname{Ad}_{(\eta,\Lambda)}^{*}\widetilde{S_{\theta}}f=\widetilde{S_{% \theta}}\widetilde{\Delta_{\theta}}^{1}((m\circ\eta)e^{(n+2)\Lambda}),$  (16) 
where $m=\widetilde{\Delta_{\theta}}f$. Applying $\widetilde{S_{\theta}^{\star}}$ to both sides of $\operatorname{Ad}_{(\eta(t),\Lambda(t))}^{*}\widetilde{S_{\theta}}f(t)=% \widetilde{S_{\theta}}f_{0}$ and using ((14)), we obtain (15). $\square$
Of course, we could also have derived (15) directly by writing the Lagrangian flow in the form
$\frac{\partial\eta}{\partial t}(t,p)=S_{\theta}f(t,\eta(t,p)),\qquad\frac{% \partial\Lambda}{\partial t}(t,p)=E(f)(t,\eta(t,p))$ 
and composing (2) with $\eta$ to obtain
$\frac{\partial}{\partial t}m(t,\eta(t,p))+(n+2)m(t,\eta(t,p))\frac{\partial% \Lambda}{\partial t}(t,p)=0,$ 
which immediately integrates to (15). But Proposition 2.7 makes clear the analogy with vorticity and momentum conservation in the general Euler–Arnold equation.
There are two significant features of the conservation law (15): the first is that the momentum is a function on the manifold rather than a vector field as it is for the EPDiff equation [Holm et al.1998] (another suggested higherdimensional version of the Camassa–Holm equation). We may thus conjecture that the sign of the momentum controls global existence of solutions as it does for the Camassa–Holm equation; see [Preston and Sarria2014] for an analysis of a closelyrelated case. The second is that the Eq. (12) can be shown to be a smooth ODE on the Sobolev manifold $\widetilde{\mathcal{D}^{s}_{\theta}}(M)$, following the methods of [Ebin1984] or [Majda and Bertozzi2002]. Thus we can avoid the somewhat complicated geometric machinery of [Ebin and Marsden1970]. We will do this in the next section.
3 Local and Global Existence
We now restrict our attention to the Hilbert manifold $\widetilde{\mathcal{D}^{s}_{\theta}}(M)$, which as noted above is a smooth submanifold of $\widetilde{\mathcal{D}^{s}}(M)=\mathcal{D}^{s}(M)\ltimes H^{s}(M)$. Our rightinvariant metric (2.3) is induced by the rightinvariant metric on $\widetilde{\mathcal{D}^{s}}(M)$, and thus we could in principle use the methods of [Ebin and Marsden1970] to prove that the tangential projection is smooth and thus that the geodesic equation is a smooth ODE on $T\widetilde{\mathcal{D}^{s}_{\theta}}(M)$. However this relies on the fact that the geodesic equation on $\widetilde{\mathcal{D}^{s}}(M)$ is a smooth ODE, which is probably true but is not proven in the literature to our knowledge. We will therefore work directly on $\widetilde{\mathcal{D}^{s}_{\theta}}(M)$ using the conservation law (12) to write the geodesic equation as a firstorder ODE on $\widetilde{\mathcal{D}^{s}_{\theta}}(M)$: we obtain
$\frac{d}{dt}(\eta,\Lambda)=(\widetilde{S_{\theta}})_{(\eta,\Lambda)}{(% \widetilde{\Delta_{\theta}})}^{{}_{1}}_{(\eta,\Lambda)}(m_{0}e^{(n+2)\Lambda% }),$  (17) 
where the “twisted operators” are defined as $(\widetilde{S_{\theta}})_{(\eta,\Lambda)}=dR_{(\eta,\Lambda)}\circ\widetilde{S% _{\theta}}\circ dR_{(\eta,\Lambda)^{1}}$ and ${(\widetilde{\Delta_{\theta}})}^{{}_{1}}_{(\eta,\Lambda)}=dR_{(\eta,\Lambda)}% \circ{(\widetilde{\Delta_{\theta}})}^{{}_{1}}\circ dR_{(\eta,\Lambda)^{1}}$. If we could prove that these twisted operators were smooth in $(\eta,\Lambda)\in\widetilde{\mathcal{D}^{s}_{\theta}}(M)$, we would be done. However although $(\widetilde{S_{\theta}})_{(\eta,\Lambda)}\colon H^{s+1}(M)\to T_{(\eta,\Lambda% )}\widetilde{\mathcal{D}^{s}}(M)$ is smooth (like all twisted firstorder differential operators, as in [Ebin and Marsden1970]), the operator ${(\widetilde{\Delta_{\theta}})}^{{}_{1}}_{(\eta,\Lambda)}$ is not, and in fact does not even map into the correct space. We need it to map from $H^{s1}(M)$ to $H^{s+1}(M)$, but it cannot map into $H^{s+1}(M)$ since $\eta$ is only $H^{s}$. Instead we use the fact that the operator $(\widetilde{S_{\theta}})_{(\eta,\Lambda)}{(\widetilde{\Delta_{\theta}})}^{{}_{% 1}}_{(\eta,\Lambda)}$ is the inverse of $\widetilde{S_{\theta}^{\star}}_{(\eta,\Lambda)}\colon T_{(\eta,\Lambda)}% \widetilde{\mathcal{D}^{s}}(M)\to H^{s1}(M)$, and $\widetilde{S_{\theta}^{\star}}_{(\eta,\Lambda)}$ is smooth in $(\eta,\Lambda)$, using a simplified version of the technique from [Ebin and Marsden1970].
We will assume the Riemannian metric on $M$ is associated to the contact form to simplify the notation, although this assumption is not necessary to prove the theorem. We assume $M$ is compact in order to use the standard results of Sobolev manifolds of maps (as in [Ebin and Marsden1970]).
Theorem 3.1.
Let $M$ be a compact contact manifold with $\dim{M}=2n+1$ and let $s$ be an integer with $s>n+\tfrac{3}{2}$. Assume the Riemannian metric on $M$ is associated to the contact form as in Definition 2.2.
Let $m_{0}$ be an arbitrary $H^{s1}$ function on $M$. Then the velocity field
$U:=(\eta,\Lambda)\mapsto(\widetilde{S_{\theta}}{(\widetilde{\Delta_{\theta}})}% ^{{}_{1}})_{(\eta,\Lambda)}(e^{(n+2)\Lambda}m_{0})$  (18) 
defined on the group $\widetilde{\mathcal{D}^{s}_{\theta}}(M)=\{(\eta,\Lambda)\in\mathcal{D}^{s}(M)% \ltimes H^{s}(M)\,\,\eta^{*}\theta=e^{\Lambda}\theta\}$ is $C^{\infty}$. Hence for any $H^{s+1}$ function $f_{0}$, there is an $H^{s}$ geodesic $(\eta(t),\Lambda(t))$ through the identity defined on some (possibly infinite) interval $(t_{b},t_{e})$ with $H^{s}$ initial velocity $(u_{0},\lambda_{0})=\widetilde{S_{\theta}}f_{0}$.
Proof.
The main idea is that firstorder twisted differential operators such as $\widetilde{S_{\theta}^{\star}}_{(\eta,\Lambda)}\colon T_{(\eta,\Lambda)}% \widetilde{\mathcal{D}^{s}}(M)\to H^{s1}(M)$ are always smooth as a function of $(\eta,\Lambda)$, as described in [Ebin and Marsden1970]. We repeat the argument here for the reader’s convenience.
We are dealing with an operator $X_{\eta}(h):=X(h\circ\eta^{1})\circ\eta$, where $h$ is an $H^{s}$ function and $X$ is a firstorder differential operator with smooth coefficients. For any such operation we have
$X_{\eta}(h)(p)=X(h\circ\eta^{1})\circ\eta\big_{p}=dh_{p}((D\eta_{p})^{1}X_{% \eta(p)})\quad\forall p\in M.$  (19) 
If $X$ is a smooth vector field, then the composition $\eta\mapsto X\circ\eta$ is smooth in $\eta$ as long as $\eta\in H^{s}$ with $s>\tfrac{1}{2}\dim{M}+1$ [Ebin1970]. In addition the operation $\eta\mapsto(D\eta)^{1}$ is smooth on the group of diffeomorphisms $\eta$ of the same Sobolev class, since it can be expressed in terms of multiplication (the cofactors) and division by a nowherezero function. Since multiplication of $H^{s1}$ functions is also smooth in each component, the expression $\eta\mapsto X_{\eta}(h)$ given by (19) is a smooth function of $\eta\in\mathcal{D}^{s}$ and $h\in H^{s}(M)$.
Recall that elements $T_{(\eta,\Lambda)}\widetilde{\mathcal{D}^{s}}(M)$ are of the form $(v,\rho)$ where $v\in H^{s}(M,TM)$ and $\rho\in H^{s}(M,\mathbb{R})$ with $v(p)\in T_{\eta(p)}M$ for each $p\in M$. We can express $v$ in terms of the frame $\{P_{k},Q_{k},E\}$ from Proposition 2.3 as
$v=aE\circ\eta+\sum_{k}[b_{k}(P_{k}\!\circ\!\eta)+c_{k}(Q_{k}\!\circ\!\eta)]$  (20) 
for some $H^{s}$ coefficient functions $\{a,b_{k},c_{k}\}$. The formal adjoint $\widetilde{S_{\theta}^{\star}}$ of $\widetilde{S_{\theta}}$ is easy to compute, and thus we find that the twisted operator
$(\widetilde{S_{\theta}^{\star}})_{(\eta,\Lambda)}=dR_{(\eta,\Lambda)}\circ% \widetilde{S_{\theta}^{\star}}\circ dR_{(\eta,\Lambda)^{1}}\colon T_{(\eta,% \Lambda)}\widetilde{\mathcal{D}^{s}}(M)\to H^{s1}(M)$ 
looks as follows:
$\begin{align}&(\widetilde{S_{\theta}^{\star}})_{(\eta,\Lambda)}(v,\rho)=a+\textstyle\sum_{k}((\operatorname{div}{Q_{k}})b_{k}(\operatorname{div}{P_{k}})c_{k})\\ &\quad\quad\quad\quadE(\rho\circ\eta^{1})\circ\eta+\textstyle\sum_{k}[Q_{k} (b_{k}\circ\eta^{1})\circ\etaP_{k}(c_{k}\circ\eta^{1})\circ\eta].\end{align}$ 
This is thus smooth in the coefficients $(a,b_{k},c_{k},\rho)\in H^{s}(M,\mathbb{R})$ by the computation above.
The restriction of each $(\widetilde{S_{\theta}^{\star}})_{(\eta,\Lambda)}$ to $T_{(\eta,\Lambda)}\widetilde{\mathcal{D}^{s}_{\theta}}(M)$ is still smooth in $(\eta,\Lambda)$ since $\widetilde{\mathcal{D}^{s}_{\theta}}(M)$ is a smooth submanifold of $\widetilde{\mathcal{D}^{s}}(M)$. On this subspace $\widetilde{S_{\theta}^{\star}}$ is an isomorphism since $\widetilde{\Delta_{\theta}}=\widetilde{S_{\theta}^{\star}}\widetilde{S_{\theta}}$ is an isomorphism from $H^{s+1}(M)$ to $H^{s1}(M)$. The operation which inverts a linear operator in a vector space is of course smooth, and thus $(\widetilde{S_{\theta}^{\star}})_{(\eta,\Lambda)}^{1}(h)=(\widetilde{S_{% \theta}}{(\widetilde{\Delta_{\theta}})}^{{}_{1}})_{(\eta,\Lambda)}(h)$ is smooth in $(\eta,\Lambda)$ for any $h\in H^{s1}(M)$. The other operations appearing in (18) involve only multiplication and composition with smooth functions, and thus the vector field $U$ is smooth on $\widetilde{\mathcal{D}^{s}_{\theta}}(M)$.
The argument in Theorem 3.1 gives existence of shorttime solutions $(\eta(t),\Lambda(t))\in\widetilde{\mathcal{D}^{s}_{\theta}}(M)$ starting at the identity $(\text{id},0)$ for any initial velocity $(u_{0},\lambda_{0})=\widetilde{S_{\theta}}f_{0}$ and any $H^{s+1}$ function $f_{0}$.
Since the curve $(\eta,\Lambda)$ is an integral curve of a smooth vector field, we have smooth dependence on time $t$, and thus the velocity $(\dot{\eta}(t),\dot{\Lambda}(t))$ is an element of $T_{(\eta,\Lambda)}\widetilde{\mathcal{D}^{s}_{\theta}}(M)$. Righttranslating to the identity, we obtain an $H^{s}$ vector field $u(t)=\dot{\eta}(t)\circ\eta(t)^{1}$ which solves the Euler–Arnold equation (2)
With this we can proceed to construct a smooth exponential map for $\widetilde{\mathcal{D}^{s}_{\theta}}(M)$, as follows.
Corollary 3.2.
Under the conditions of Theorem 3.1, there is a smooth Riemannian exponential map which takes sufficiently small tangent vectors $\widetilde{S_{\theta}}f_{0}\in T_{\text{id}}\widetilde{\mathcal{D}^{s}_{\theta% }}(M)$ to the timeone solution $(\eta(1),\Lambda(1))\in\widetilde{\mathcal{D}^{s}_{\theta}}(M)$. By the inverse function theorem on Hilbert manifolds, this exponential map is locally invertible. Hence sufficiently close elements of $\widetilde{\mathcal{D}^{s}_{\theta}}(M)$ may be joined by a unique minimizing unitspeed geodesic.
Proof.
To obtain this map, we examine the dependence of $(\eta(t),\Lambda(t))$ on its initial data. First we note that if
$\widetilde{U}:=(\eta,\Lambda,u_{0},\lambda_{0})\mapsto(\widetilde{S_{\theta}}{% (\widetilde{\Delta_{\theta}})}^{{}_{1}})_{(\eta,\Lambda)}(e^{(n+2)\Lambda}m_% {0})$  (21) 
as in (18), then $\widetilde{U}$ is smooth in all its arguments, so for any $t$, $(\eta(t),\Lambda(t))$ is a smooth function of $(u_{0},\lambda_{0},t).$ This function is defined on a neighborhood of $(\tilde{0},0)$ in $T_{id}\widetilde{\mathcal{D}^{s}_{\theta}}(M)\times\mathbb{R}$ where $\tilde{0}$ is the zero vector in $T_{id}\widetilde{\mathcal{D}^{s}_{\theta}}(M)$. Thus there is a ball $B_{2\delta}$ about $\tilde{0}$ of radius $2\delta$ and an interval $(\epsilon,\epsilon)$ such that $(\eta(t),\Lambda(t))$ the solution of (18), with initial data in $B_{2\delta}$, is defined for $t\in(\epsilon,\epsilon).$ But since $(\eta(t),\Lambda(t))$ is a geodesic, we find that for any fixed $r$, $t\rightarrow(\eta(rt),\Lambda(rt))$ is also a geodesic which of course is defined for $t<\epsilon/r.$ Hence for any initial vector in $B_{\delta r},$ we get a geodesic defined for $t<2.$ The value of the exponential map is then defined to be $(\eta(1),\Lambda(1)).$ $\square$
Of course there is an isomorphism between $\widetilde{\mathcal{D}_{\theta}}(M)$ and $\mathcal{D}_{\theta}(M)$ (obtained by simply forgetting about the scaling $\Lambda$), and we may thus use this result to discuss the Riemannian exponential map directly on the contactomorphism group $\mathcal{D}_{\theta}(M)$, if desired. The extension to $\widetilde{\mathcal{D}^{s}_{\theta}}(M)$ is only to make the technical details work out more easily.
We have used the conservation law in Proposition 2.7 to prove local existence of solutions; it also implies that the only thing that can go wrong with global existence is that $\eta$ fails to be a diffeomorphism because the Jacobian determinant $\operatorname{Jac}{(\eta)}$ approaches zero or infinity in finite time. This is the same behavior one sees in a typical onedimensional nonlinear hyperbolic equation. Intuitively we expect that as long as $\operatorname{Jac}{(\eta)}$ satisfies an estimate of the form $0<a\leq\operatorname{Jac}{(\eta(t))}\leq b$ for $0\leq t\leq T$, then the momentum $m(t)$ will be a globally bounded function. Since $m(t)=f(t)\Delta f(t)$, a $C^{0}$ bound on $m$ roughly implies a $C^{2}$ bound on $f$, which leads to estimates on all Sobolev norms of the velocity field $u$ as in [Beale et al.1984]. Since $\operatorname{Jac}{(\eta)}=\exp{[(n+1)\Lambda]}$ for any $(\eta,\Lambda)\in\widetilde{\mathcal{D}_{\theta}}(M)$ by Lemma 2.6, we can write the global existence condition in terms of the function $\Lambda$, and this gives a “Beale–Kato–Majda”style criterion for global existence as in [Beale et al.1984]. As before we will work with an associated Riemannian metric just to simplify the notation, though the result does not depend on this assumption.
Theorem 3.3.
Let $M$ be a compact contact manifold of dimension $2n+1$ as in Theorem 3.1 with associated Riemannian metric. Let $(u(t),\lambda(t))=\widetilde{S_{\theta}}f(t)$ be a solution of the Euler–Arnold equation (2) (defined a priori only for short time) with $f(t)\in H^{s+1}(M)$ for some $s>n+3/2$. Then the solution exists up to time $T$ if we have
$\int_{0}^{T}\lVert E(f)(t)\rVert_{L^{\infty}}\,dt=C<\infty\qquad\text{for all % }\,\,t\in[0,T].$  (22) 
Proof.
Since the solution $(u(t),\lambda(t))$ exists as long as $(\eta(t),\Lambda(t))$ does, and since $(\eta(t),\Lambda(t))$ solves a smooth ordinary differential equation on $\widetilde{\mathcal{D}^{s}_{\theta}}(M)$, it is sufficient to show that $\lVert u(t)\rVert_{H^{s}}$ and $\lVert\lambda(t)\rVert_{H^{s}}$ remain bounded; hence it is sufficient to show that $\lVert f(t)\rVert_{H^{s+1}}$ is bounded on $[0,T]$, where $f(t)$ is the stream function. We will use the conservation law (15) to achieve this.
First we note that since $\operatorname{Jac}{(\eta)}=e^{(n+1)\Lambda}$ by Lemma 2.6 and $\Lambda$ satisfies $\frac{\partial}{\partial t}\Lambda(t,x)=E(f)(t,\eta(t,x))$, our assumption (22) implies that
$e^{(n+1)C}\leq\operatorname{Jac}{\eta(t)}\leq e^{(n+1)C}.$ 
Using (15), we obtain that $\lvert m(t,\eta(t,p))\rvert\leq\lvert m_{0}(p)\rvert e^{(n+2)C}$ for all $p\in M$, and in particular $\lVert m(t)\rVert_{C^{0}}\leq e^{(n+2)C}\lVert m_{0}\rVert_{C^{0}}$. Using this we will find a bound for $df(t)$, or equivalently for $\widetilde{S_{\theta}}f(t)$.
Recall from Proposition 2.3 that the contact Laplacian $\widetilde{\Delta_{\theta}}$ is an isomorphism from $H^{s+1}(M)$ to $H^{s1}(M)$. From the theory of elliptic operators ([Taylor1996], Chapter 7, Proposition 2.2 for $M=\mathbb{R}^{n}$ and Chapter 7, Section 12 for $M$ any compact manifold) we find that its inverse is a pseudodifferential operator whose Schwartz kernel $k:M\times M\rightarrow\mathbb{R}$ is smooth off the diagonal and obeys the estimate
$D_{p}^{\beta}k(p,q)\leq K\delta(p,q)^{2n+1\beta}\quad{\rm for}\quad 2n+% \beta>1,$  (23) 
where $D_{p}^{\beta}$ means a $\beta$order derivative operator with respect to the first variables of $k$ and $\delta(p,q)$ is the distance from $p$ to $q$ defined by the Riemannian metric on $M$.^{1}^{1}In the inequalities that follow $K$ will always denote some positive constant, but it may be different in different inequalities.
From this and the fact that $m=\widetilde{\Delta_{\theta}}f=f\Delta f$, we can estimate
$f(p)=\int_{M}k(p,q)m(q)\,d\mu(q)$ 
and
$df(p)=\int_{M}d_{p}k(p,q)m(q)d\mu(q)$  (24) 
where $d_{p}$ is the differential with respect to the $p$variables and $d\mu(q)$ indicates integration with respect to $q$ using the Riemannian volume element of $M$.^{2}^{2}In the sequel we will sometimes write $dk$ for $d_{p}k.$ We have $k(p,q)\leq K\delta(p,q)^{2n+1}$ and $d_{p}k(p,q)\leq K\delta(p,q)^{2n},$ so both of these integrals are bounded by a constant times $\m(t)\_{C^{0}}$ which, as we have seen, is bounded in time. With this and formula (4) we see that $u=S_{\theta}f$ is bounded uniformly in time as well.
We proceed to seek a timeuniform Lipschitz bound for $df$, but in fact we will be able to find only a quasiLipschitz bound, as we shall now explain. Since $M$ is compact, we can find a positive $\epsilon$ such that each point of $M$ has a normal coordinate neighbourhood ball of radius at least $\epsilon.$
Fix $p\in M$. Then for any $q\in M$ with $\delta(p,q)<\epsilon$, we have a unique minimal geodesic $\chi$ parameterized so that $\chi(0)=p$ and $\chi(1)=q$. Fix such a $q$. We let $b=\chi^{\prime}(1),$ so that $b=\delta(p,q)$. Also we parallel translate $df(p)$ along $\chi$ to get some $df^{\prime}(q)\in T^{*}_{q}M.$ Then we shall estimate $df(q)df^{\prime}(q)$ where $\;\>$ is the norm on $T^{*}_{q}M.$ To do this we use the formula (24) for $df$, and we parallel translate each $d_{p}k(p,r)$ for $r\in M$ along $\chi$ to get $dk^{\prime}(q,r)\in T^{*}_{q}M.$ In this way we get
$df^{\prime}(q)=\int_{M}dk^{\prime}(q,r)m(r)\,d\mu(r)$ 
and we find
$df^{\prime}(q)df(q)=\int_{M}(dk^{\prime}(q,r)dk(q,r))m(r)\,d\mu(r)$ 
Following [Kato1967], Lemma 1.4, we split up this integral as follows: Let $\Sigma=B_{2b}(p),$ the ball of radius $2b$ about $p$. Then $\int_{M}=\int_{\Sigma}+\int_{M\backslash\Sigma}$. For the integral over $\Sigma$, we have the estimate
$\int_{\Sigma}dk^{\prime}(q,r)m(r)\,d\mu(r)\leq K\lVert m\rVert_{C^{0}}\int_{% \Sigma}\delta(p,r)^{2n}\,d\mu(r)\leq 2bK\lVert m\rVert_{C^{0}}.$ 
Also $\Sigma\subset B_{3b}(q)$ and
$\int_{\Sigma}dk(q,r)m(r)\,d\mu(r)\leq K\lVert m\rVert_{C^{0}}\int_{\Sigma}% \delta(q,r)^{2n}\,d\mu(r)\leq 3bK\lVert m\rVert_{C^{0}}.$ 
Combining these we get
$\int_{\Sigma}(dk^{\prime}(q,r)dk(q,r))m(r)\,d\mu(r)\leq 5bK\lVert m\rVert_{C^% {0}}.$  (25) 
The estimate of the integral over $M\backslash\Sigma$ is more subtle. If we let $P(\tau)$ denote parallel translation along $\chi$ from $\chi(\tau)$ to $\chi(1)$, so that $P(\tau):T^{*}_{\chi(\tau)}M\rightarrow T^{*}_{q}M,$ we find that
$\displaystyle dk^{\prime}(q,r)dk(q,r)$  $\displaystyle=P(0)(dk(p,r))P(1)(dk(q,r))$  
$\displaystyle=\int_{0}^{1}P(\tau)\nabla_{\chi^{\prime}(\tau)}dk(\chi(\tau),r)% \,d\mu(r).$ 
Since parallel translation is an isometry, we therefore have
$\displaystyledk^{\prime}(q,r)dk(q,r)$  $\displaystyle\leq\max_{0\leq\tau\leq 1}\{\nabla_{\chi^{\prime}(\tau)}dk(\chi(% \tau),r)\}$  
$\displaystyle\leq K\max_{0\leq\tau\leq 1}\lvert\chi^{\prime}(\tau)\rvert\delta% (\chi(\tau),r)^{2n1}.$ 
Now $\lvert\chi^{\prime}(\tau)\rvert=b$ for all $\tau$, and by the triangle inequality we have for all $\tau\in[0,1]$ that
$\delta(\chi(\tau),r)\geq\delta(p,r)\delta(p,\chi(\tau))\geq\delta(p,r)b.$ 
We conclude that
$\lvert dk^{\prime}(q,r)dk(q,r)\rvert\leq Kb\lvert\delta(p,r)b\rvert^{2n1}$ 
whenever $r\in M\backslash\Sigma$, for any $q$ such that $\delta(p,q)=b<\epsilon$.
Let $R={\rm diam}(M)<\infty$ (since $M$ is compact). Then
$\displaystyle\int_{M\backslash\Sigma}dk^{\prime}(q,r)dk(q,r)\,d\mu(r)$  $\displaystyle\leq Kb\int_{M\backslash\Sigma}(\delta(p,r)b)^{2n1}d\mu(r)$  
$\displaystyle\leq Kb\int_{2b}^{R}\frac{\rho^{2n}}{(\rhob)^{2n+1}}\,d\rho$ 
(possibly modifying $K$). For $2b\leq\rho\leq R$ we know that $1\leq\frac{\rho}{\rhob}\leq\frac{3}{2}$, so we can overestimate
$\int_{M\backslash\Sigma}dk^{\prime}(q,r)dk(q,r)\,d\mu(r)\leq K^{\prime}b% \int_{2b}^{R}(\rhob)^{1}\,d\rho\leq K^{\prime}b\log{(R/b)}.$ 
Combining this with (25) we find
$\int_{M}dk^{\prime}(q,r)dk(q,r)\,d\mu(r)\leq 5K\delta(p,q)+K^{\prime}\delta% (p,q)\log(R/\delta(p,q))$ 
for $\delta(p,q)<\epsilon.$ By increasing $K$ and $K^{\prime}$ we simplify this inequality to
$\int_{M}dk^{\prime}(y,z)dk(y,z)\,d\mu(r)\leq K\delta(p,q)(1+\log(R/\delta(p% ,q)).$ 
Thus we find that if $\delta(p,q)<\epsilon$ and $df^{\prime}(q)$ is the parallel transport of $df(p)$ along the minimizing geodesic from $p$ to $q$, then
$df^{\prime}(q)df(q)\leq K\delta(p,q)(1+\log(R/\delta(p,q))$  (26) 
where $K$ is independent of $t$ as before. With this inequality we say that $df$ is quasiLipschitz. Also since $df(p)$ is bounded independently of $p$ and $t$ we find that by further increasing $K$ we get (26) for all $p,q\in M;$ that is, we can drop the restriction $\delta(p,q)<\epsilon.$ As a consequence note that for any $\gamma<1$ we have
$\lvert df^{\prime}(q)df(q)\rvert\leq K\delta(p,q)^{\gamma}$  (27) 
since the logarithm grows slower than any power. Hence $df$ is uniformly $C^{\gamma}$ for any $\gamma<1$.
Since $u=S_{\theta}f$, our bound for $df$ gives the same quasiLipschitz bound for $u$, again uniformly in $t$. Using this bound we can find a positive $\alpha$ for which the flow $\eta(t)$ of $u(t)$ is $C^{\alpha}.$ However we also need to show that $\eta(t)^{1}$ is $C^{\alpha}$. Fortunately we can do this by the same method: given any fixed $t_{0}\in[0,T)$, we define a time dependent vector field $v$ on $M$ by $v(t)=u(t_{0}t)$. Then if $\sigma$ is the flow of $v$, it is easy to see that the maps $t\mapsto\sigma(t,\eta(t_{0},x))$ and $t\mapsto\eta(t_{0}t,x)$ satisfy the same differential equation, and since $\sigma(0,\eta(t_{0},x))=\eta(t_{0},x)$, they must be equal for all times $t\in[0,t_{0}]$. Hence in particular $\sigma(t_{0})=\eta(t_{0})^{1}.$ We proceed to show that $\sigma(t_{0})$ is $C^{\alpha}$ for some $\alpha>0$; the fact that each $\eta(t)$ is $C^{\alpha}$ is similar.
Fix $p$ and $q$ in $M$. Let $\chi\colon[0,t_{0}]\times[0,1]$ be the map such that for each $t\in[0,t_{0}]$, the curve $\tau\mapsto\chi(t,\tau)$ is the minimal geodesic between $\sigma(t,p)$ and $\sigma(t,q)$ with $\chi(t,0)=\sigma(t,p)$ and $\chi(t,1)=\sigma(t,q)$. Define
$\phi(t)=\delta(\sigma(t,p),\sigma(t,q))=\int_{0}^{1}\Big\lvert\frac{\partial% \chi}{\partial\tau}(t,\tau)\Big\rvert\,d\tau.$ 
Then
$\displaystyle\phi^{\prime}(t)$  $\displaystyle=\frac{d}{dt}\left(\int_{0}^{1}\Big\lvert\frac{\partial\chi}{% \partial\tau}(t,\tau)\Big\rvert\,d\tau\right)$  
$\displaystyle=\int_{0}^{1}\frac{1}{\Big\lvert\frac{\partial\chi}{\partial\tau}% (t,\tau)\Big\rvert}\,\left\langle\frac{\partial\chi}{\partial\tau}(t,\tau),% \frac{D}{\partial t}\frac{\partial\chi}{\partial\tau}(t,\tau)\right\rangle\,d\tau$ 
But $\tfrac{D}{\partial t}\tfrac{\partial\chi}{\partial\tau}=\tfrac{D}{\partial\tau% }\tfrac{\partial\chi}{\partial t}$ by general properties of surface maps (e.g., [Lang1999], Chapter XIII, Lemma 5.3), and $\tfrac{D}{\partial\tau}\tfrac{\partial\chi}{\partial\tau}=0$ since each $\tau\mapsto\chi(t,\tau)$ is a geodesic, and thus an integration by parts yields
$\phi^{\prime}(t)=\frac{1}{\left\lvert\tfrac{\partial\chi}{\partial\tau}(t,\tau% )\right\rvert}\Big\langle\frac{\partial\chi}{\partial\tau}(t,\tau),\frac{% \partial\chi}{\partial t}(t,\tau)\Big\rangle\Big_{\tau=0}^{\tau=1},$ 
using the fact that $\lvert\tfrac{\partial\chi}{\partial\tau}(t,\tau)\rvert$ is constant in $\tau$ since $\chi$ is a geodesic in $\tau$.
Now $\frac{\partial\chi}{\partial\tau}$ is parallel along $\chi$, and since the parallel transport $P$ from $\chi(0)$ to $\chi(1)$ preserves inner products, we have
$\left\langle\tfrac{\partial\chi}{\partial\tau}(t,0),v(t,\sigma(t,p))\right \rangle=\left\langle\tfrac{\partial\chi}{\partial\tau}(t,1),Pv(t,\sigma(t,p)) \right\rangle.$ 
Thus
$\displaystyle\phi^{\prime}(t)$  $\displaystyle=\frac{1}{\left\lvert\tfrac{\partial\chi}{\partial\tau}(t,\tau)% \right\rvert}\bigg\langle\tfrac{\partial\chi}{\partial\tau}(t,1),v(t,\sigma(t,% q))Pv(t,\sigma(t,p))\bigg\rangle$  
$\displaystyle\leq\lvert v(t,\sigma(t,q))Pv(t,\sigma(t,p))\rvert.$ 
Now since $v$ like $u$ is quasiLipschitz on $[0,t_{0}]$, we have a constant $K$ such that
$\phi^{\prime}(t)\leq K\phi(t)\left(1+\log\left(\frac{R}{\phi(t)}\right)\right),$  (28) 
where the constants $R$ and $K$ do not depend on $t$ or $t_{0}$.
We proceed to estimate $\phi(t)$. Let $\psi(t)=\log(\phi(t)/R)$ so $\psi^{\prime}=\phi^{\prime}/\phi.$ Then from (28) we get $\psi^{\prime}\leq K(1\psi)$. Integrating this we find
$\psi(t)\leq\psi(0)e^{Kt}+1e^{Kt}.$ 
Exponentiating this inequality and noting that $\phi(0)\leq R$ we find that
$\frac{\phi(t)}{R}\leq\left(\frac{\phi(0)}{R}\right)^{e^{Kt}}e^{1e^{Kt}}\leq% \left(\frac{\phi(0)}{R}\right)^{e^{KT}}e$ 
Thus $\phi(t)\leq R^{1e^{KT}}e\phi(0)^{e^{KT}}$, so letting $\alpha=e^{KT}$ and $L=eR^{1e^{KT}}$, we get $\phi(t)\leq L\phi(0)^{\alpha}$ and hence
$\delta(\sigma(t_{0},p),\sigma(t_{0},q))\leq L\delta(p,q)^{\alpha}.$  (29) 
The constants $L$ and $\alpha$ do not depend on the choice of $t_{0}$, so the estimate (29) holds for all $t_{0}\in[0,T)$. From (29) and the conservation law from Proposition 2.7 in the form
$m(t,p)=m_{0}(\sigma(t,p))\exp{[(n+2)\Lambda(t,\sigma(t,p)))]},$ 
we conclude that $m$ is Hölder continuous as follows: since $df$ is $C^{\gamma}$ for any $\gamma$, so is $E(f)$, and thus $\Lambda(t,p)=\int_{0}^{t}E(f)(\tau,\eta(\tau,p))\,d\tau$ is Hölder continuous as a composition of Hölder continuous functions. Now $\Lambda\circ\sigma$ and $m_{0}\circ\sigma$ are also Hölder continuous since $\sigma$, $\Lambda$, and $m_{0}$ are. Finally the product of Hölder continuous functions is still Hölder continuous (for a possibly smaller exponent), so we find that $m(t)$ is bounded uniformly in $t$ in $C^{\alpha}(M,\mathbb{R})$ for some $\alpha>0$, and thus by standard elliptic theory we get $f(t)$ bounded in $C^{2+\alpha}(M,\mathbb{R})$, from which it follows that $S_{\theta}f$ is bounded in $C^{1+\alpha}(TM)$.
We now need a $C^{1}$ bound on $m(t)=\widetilde{\Delta_{\theta}}f(t)$, which we obtain as follows: computing the gradient of both sides of (2), we have
$\nabla m_{t}+\nabla_{u}\nabla m+[\nabla,\nabla_{u}]m+(n+2)m\nabla E(f)+(n+2)E(% f)\nabla m=0,$ 
which implies that
$\displaystyle\frac{d}{dt}\lvert\nabla m(t,\eta(t,x))\rvert$  $\displaystyle\leq\lvert[\nabla,\nabla_{u}]m\rvert(t,\eta(t,x))$  
$\displaystyle\qquad\qquad+(n+2)\lvert m(t,\eta(t,x))\rvert\lvert\nabla E(f)(t,% \eta(t,x))$  
$\displaystyle\qquad\qquad+(n+2)\lvert E(f)(t,\eta(t,x))\rvert\lvert(\nabla m)(% t,\eta(t,x))\rvert$  
$\displaystyle\leq K\lVert u(t)\rVert_{C^{1}}\lVert m(t)\rVert_{C^{1}}$  
$\displaystyle\qquad\qquad+(n+2)\lVert m(t)\rVert_{C^{0}}\lVert f(t)\rVert_{C^{% 2}}$  
$\displaystyle\qquad\qquad+(n+2)\lVert f(t)\rVert_{C^{1}}\lVert m(t)\rVert_{C^{% 1}}.$ 
Gronwall’s inequality then implies that
$\lVert m(t)\rVert_{C^{1}}\leq\lVert m_{0}\rVert_{C^{1}}\exp{\left(K\int_{0}^{t% }\lVert f(\tau)\rVert_{C^{2}}\,d\tau\right)}$ 
for some constant $K$, and since $f(t)$ is bounded in $C^{2+\alpha}$, we know it is also bounded in $C^{2}$; thus $m(t)$ is bounded in $C^{1}$.
Now we show that $f(t)$ is bounded in the $H^{s+1}$ topology, or equivalently that $m(t)=\widetilde{\Delta_{\theta}}f(t)$ is bounded in $H^{s1}.$ Since $\partial_{t}m=u(m)(n+2)mE(f)$, for $s=1$ we have
$\displaystyle\frac{d}{dt}\int_{M}m^{2}\mu$  $\displaystyle=\int_{M}u(m^{2})\,d\mu2(n+2)\int_{M}m^{2}E(f)\,d\mu$  
$\displaystyle=\int_{M}m^{2}(\operatorname{div}{u}(2n+4)E(f))\,d\mu$  
$\displaystyle=(n+3)\int_{M}m^{2}E(f)\,d\mu,$ 
using (8), so that
$\int_{M}m(t)^{2}\,d\mu\leq e^{(n+3)C}\int_{M}m_{0}^{2}\,d\mu.$ 
If $s>1$, then taking $s1$ spatial derivatives^{3}^{3}Powers of $\nabla$ are defined in a standard way: for any function $f,$ $\nabla f$ is a section of $TM$, $\nabla^{2}f$ is a section of $TM\otimes T^{*}M$ and for any $k$, $\nabla^{k}f$ is a section of $TM\otimes(T^{*}M)^{k1}$. Inner products are defined by the induced Riemannian metric. we get
$\begin{align}\frac{d}{dt}\int_{M}\nabla^{s1}m^{2}\mu=&2\int_{M}\langle\nabla_{u}\nabla ^{s1}m,\nabla^{s1}m\rangle\,d\mu\\ &2(n+2)\int_{M}E(f)\langle\nabla^{s1}m,\nabla^{s1}m\rangle\,d\mu\\ &2\int_{M}\langle[\nabla^{s1},\nabla_{u}]m,\nabla^{s1}m\rangle\,d\mu\\ &2(n\!+\!2)\int_{M}\langle\nabla^{s1}m,[\nabla^{s1},E(f)]\nabla^{s1}m% \rangle\,d\mu,\quad\end{align}$ 
where $[\;,\;]$ denotes the commutator.
As before, the first two terms in (3) reduce to
$(n+3)\int_{M}E(f)\lvert\nabla^{s1}m\rvert^{2}\,d\mu,$ 
and for the last two terms we use the standard estimate
$\\nabla^{k}(hg)h\nabla^{k}g\_{H^{0}}\leq K(\h\_{H^{k}}\g\_{C^{0}}+\% \nabla h\_{C^{0}}\g\_{H^{k1}}),$  (30) 
(with $k=s1$) which can be found in (Taylor1996], Chapter 13, Proposition 3.7). For the first commutator we choose $h=u$ and $g=\nabla m$ and obtain
$\begin{align}&\int_{M}\langle[\nabla^{s1},\nabla_{u}]m,\nabla^{s1}m\rangle\mu\\ &\quad\leq K(\lVert u\rVert_{H^{s1}}\lVert m\rVert_{C^{1}}+\u\_{C^{1}}\m \_{H^{s1}})\lVert m\rVert_{H^{s1}}.\end{align}$ 
We already have bounds for $\lVert m(t)\rVert_{C^{1}}$ and for $\lVert u(t)\rVert_{C^{1}}$, and since $\lVert u(t)\rVert_{H^{s1}}\lesssim\lVert m(t)\rVert_{H^{s2}}$ we have a bound for the first commutator in terms of $\lVert m(t)\rVert^{2}_{H^{s1}}$.
To bound the second commutator in (3), we use (30) again with $h=E(f)$ and $g=m$ to obtain
$\begin{align}&\int_{M}\langle\nabla^{s1}m,[\nabla^{s1},E(f)]\nabla^{s1}m\rangle\,d\mu\\ &\quad\leq\tilde{K}(\lVert f\rVert_{H^{s}}\lVert m\rVert_{C^{0}}+\lVert f \rVert_{C^{2}}\lVert m\rVert_{H^{s2}})\lVert m\rVert_{H^{s1}},\end{align}$ 
and we already have bounds for each of these. Combining and overestimating, we obtain
$\frac{d}{dt}\lVert\nabla^{s1}m\rVert^{2}_{L^{2}}\leq(n+3)\lVert E(f)\rVert_{C% ^{0}}\lVert\nabla^{s1}m\rVert_{L^{2}}^{2}+\overline{K}\lVert m\rVert_{C^{1}}% \lVert m\rVert^{2}_{H^{s1}},$ 
which leads to a bound on $\lVert m(t)\rVert_{H^{s1}}$ on $[0,T]$ by Gronwall’s inequality. This completes the proof. $\square$
In the next section we will analyze a special case where one can obtain global existence essentially for free.
4 Special Cases and Other Aspects
4.1 Quantomorphisms
In some situations we care more about the contact form than the contact structure. In this case the appropriate group to consider is the group of quantomorphisms given by
$\mathcal{D}_{q}(M)=\{\eta\in\mathcal{D}(M)\,\,\eta^{*}\theta=\theta\}.$ 
We may identify this group with the subgroup
$\{(\eta,\Lambda)\in\widetilde{\mathcal{D}_{\theta}}(M)\,\,\Lambda=0\}.$ 
Every quantomorphism preserves the volume form by Lemma 2.6. A quantomorphism also preserves the Reeb field: infinitesimally if $E(f)=0$ and $u=S_{\theta}f$, then
$[E,u]=[S_{\theta}1,S_{\theta}f]=S_{\theta}\{1,f\}=S_{\theta}(E(f))=0$ 
by (5); the noninfinitesimal proof works as in [Ratiu and Schmid1981]. As a result we have
$T_{\text{id}}\mathcal{D}_{q}(M)=\{S_{\theta}f\,\,E(f)\equiv 0\}.$  (31) 
The “padded quantomorphism group,” viewed as a subgroup of the padded contactomorphism group, consists of
$\widetilde{\mathcal{D}_{q}}(M)=\{\widetilde{S_{\theta}}f\,\,E(f)\equiv 0\}=\{% (S_{\theta}f,0\}\,\,E(f)\equiv 0\}.$ 
The following example shows that the quantomorphism group structure depends greatly on the properties of the Reeb field.
Example 4.1.
On $M=\mathbb{T}^{3}=(\mathbb{R}/2\pi\mathbb{Z})^{3}$ with coordinates $(x,y,z)$ and with contact form $\theta=\sin{z}\,dx+\cos{z}\,dy$, the Reeb field is $E=\sin{z}\,\partial_{x}+\cos{z}\,\partial_{y}$. Every quantomorphism must preserve the Reeb field, but the Reeb field has nonclosed orbits whenever $\tan{z}$ is irrational, and hence any function which is constant on the orbits must actually be a function only of $z$. It is then easy to see that the identity component of $\mathcal{D}_{q}(\mathbb{T}^{3})$ consists of diffeomorphisms of the form
$\eta(x,y,z)=(x+p(z)\sin{z}+p^{\prime}(z)\cos{z},y+p(z)\cos{z}p^{\prime}(z)% \sin{z},z)$ 
for some function $p\colon S^{1}\to\mathbb{R}$. This group is abelian, so any rightinvariant metric will actually be biinvariant, and all geodesics will be oneparameter subgroups.
The only way to get an interesting quantomorphism group is if the Reeb field happens to have all of its orbits closed and of the same length. In this case the contact manifold must be related to a symplectic manifold by a Boothby–Wang fibration [Boothby and Wang1958]. We say that the contact form is regular, following [Ratiu and Schmid1981]. If this happens, then there is a symplectic manifold $N$ given as the quotient space of $M$ by the orbits, with a map $\pi\colon M\to N$ and a symplectic form $\omega$ on $N$ such that $\pi^{*}\omega=d\theta$. The bestknown example is the Hopf fibration of $S^{3}$ over $S^{2}$. When the contact form is regular, the tangent space to $\mathcal{D}_{q}(M)$ may be identified with the space of functions $f\colon M\to\mathbb{R}$ such that $E(f)=0$.
[Omori1974] proved (Theorem 8.4.2) that if $\theta$ is regular, then $\mathcal{D}^{s}_{q}(M)$ is a smooth Hilbert submanifold of $\widetilde{\mathcal{D}^{s}_{\theta}}(M)$. Hence the Riemannian metric (2.3) induces a Riemannian metric on $\mathcal{D}^{s}_{q}(M)$, and the geodesic equation on the submanifold is obtained by the tangential projection of the full geodesic equation (2) on $\widetilde{\mathcal{D}^{s}_{\theta}}(M)$. We now prove that this submanifold is totally geodesic by showing that the second fundamental form vanishes.
Proposition 4.2.
Suppose $M$ is a contact manifold with an associated Riemannian metric as in Definition 2.2, and suppose that the Reeb field $E$ is a Killing field. If $\theta$ is a regular contact form on $M$, then $\widetilde{\mathcal{D}_{q}}(M)$ is a totally geodesic submanifold of $\widetilde{\mathcal{D}_{\theta}}(M)$. Hence any solution of the Euler–Arnold equation (2)(2) that $\{f,g\}=u(g)$ where $u=S_{\theta}f$, so that
$\langle\!\langle\tilde{u},\operatorname{ad}_{\tilde{u}}\tilde{v}\rangle\!% \rangle=\int_{M}mu(g)\,d\mu=\int_{M}g\operatorname{div}{(mu)}\,d\mu=\int_{M}% gu(m)\,d\mu,$ 
since $\operatorname{div}{u}=(n+1)E(f)=0$ by Proposition 2.3.
Now $g$ is orthogonal to any function which is Reebinvariant, so we will have $\langle\!\langle\tilde{u},\operatorname{ad}_{\tilde{u}}\tilde{v}\rangle\!% \rangle=0$ for $\tilde{v}=\widetilde{S_{\theta}}g$ as long as we know $E(u(m))=0$ whenever $m=\widetilde{\Delta_{\theta}}f$ and $u=S_{\theta}f$ for an $f$ with $E(f)=0$. Since $E=S_{\theta}1$, we have
$\displaystyle E(u(m))$  $\displaystyle=S_{\theta}1(S_{\theta}f(m))$  
$\displaystyle=[S_{\theta}1,S_{\theta}f](m)+S_{\theta}f(S_{\theta}1(m))$  
$\displaystyle=S_{\theta}\{1,f\}(m)+S_{\theta}f(E(m)).$ 
Now by formula (5) we have $\{1,f\}=S_{\theta}1(f)fE(1)=E(f)=0$, and since $E$ commutes with $\widetilde{\Delta_{\theta}}$ we have $E(m)=E(\widetilde{\Delta_{\theta}}(f))=\widetilde{\Delta_{\theta}}(E(f))=0$. We conclude that $\langle\!\langle\tilde{u},\operatorname{ad}_{\tilde{u}}\tilde{v}\rangle\!% \rangle=0$, and thus the second fundamental form of $\widetilde{\mathcal{D}_{q}}(M)$ is zero. $\square$
Proposition 4.2 has the easy corollary that if the contact form is regular, any solution of the Euler–Arnold equation (2) for which $E(f_{0})=0$ will automatically have global solutions in time, using Theorem 3.3.
Corollary 4.3.
Suppose $M$ is a compact contact manifold with associated Riemannian metric satisfying Definition 2.2, and such that the contact form $\theta$ is regular with the Reeb field $E$ a Killing field of the metric. Then any solution of (2) such that $E(f_{0})\equiv 0$ will have $E(f(t))=0$ whenever it is defined, and hence by Theorem 3.3 the solution will exist for all time.
If $M$ is threedimensional (so that the Boothby–Wang quotient is twodimensional, and its volume form is the symplectic form), the Euler–Arnold equation on the quantomorphism group takes the form
$m_{t}+\{f,m\}=0,\qquad m=f\Delta f,$  (32) 
where $\{\cdot,\cdot\}$ is the standard Poisson bracket. We may rescale the metric on $M$ so that the Reeb field has a different constant length $\alpha$, and in this case the momentum takes the form $m=\alpha^{2}f\Delta f$. Thus the Euler–Arnold equation on the quantomorphism group of $M$ is the quasigeostrophic equation in $f$plane approximation on $N$, as in [Holm and Zeitlin1998] and [Zeitlin and Pasmanter1994]; here $\alpha^{2}$ is the Froude number.
An alternative approach to the quantomorphism group is to view it as a central extension of the group $\mathcal{D}_{\text{Ham}}(N)$ of Hamiltonian diffeomorphisms of the symplectic manifold $N$; this approach is used in [Ratiu and Schmid1981] and is also taken in the references [Holm and Tronci2009], [GayBalmaz and Vizman2012] and [GayBalmaz and Tronci2012]. [Smolentsev1994] computed the curvature tensor of the quantomorphism group under the same assumptions.
A more sophisticated version of the quasigeostrophic equation is the $\beta$plane approximation, for which the evolution equation for $f(t,x,y)$ takes the form
$(\alpha^{2}f+\Delta f)_{t}+\{f,\Delta f\}+\beta\partial_{x}f=0,$  (33) 
where $\alpha$ and $\beta$ are constants. [Vizman2008] derived this equation as the Euler–Arnold equation of a central extension of the group of Hamiltonian diffeomorphisms, in the case that $\alpha=0$. However the same central extension applied to the group of quantomorphisms yields (33). We can obtain global existence for these equations in exactly the same way as in Theorem 3.3, since there is a potential vorticity which is transported and there is no stretching.
Explicitly, given a Reebinvariant function $\psi$ on $M$, and two Reebinvariant functions $p$ and $q$ on $M$ such that the contact bracket satisfies^{4}^{4}All such functions descend to the Boothby–Wang quotient $N$, so that all we want is that $\{\overline{p},\overline{q}\}=\overline{\psi}$ for the standard Poisson bracket on $N$, where $\overline{p}$, $\overline{q}$, and $\overline{\psi}$ are the quotient functions on $N$. $\{p,q\}=\psi$, let us define a cocycle on $\mathcal{D}_{q}(M)$ by the formula
$B(\eta,\xi)=\int_{M}p(q\circ\eta+q\circ\xiq\circ\eta\circ\xiq)\,d\mu.$  (34) 
The corresponding cocycle on the Lie algebra is
$b(u,v)=\int_{M}p[u,v](q)\,d\mu,$  (35) 
and $p$ and $q$ are related by $\{p,q\}=\psi$.
Proposition 4.4.
If $M$ is a contact manifold with an associated metric and a regular contact form, and $N$ is its Boothby–Wang quotient with the Riemannian metric prescribed so that the projection $\pi\colon M\to N$ is a Riemannian submersion, then on the Lie algebra $T_{\text{id}}G$ consisting of $T_{\text{id}}\mathcal{D}_{q}(M)$ with central extension defined by (35), the Euler–Arnold equation $\dot{u}+\operatorname{ad}_{u}^{*}u=0$ reduces to
$\omega_{t}+\{\overline{f},\omega\}=0,\qquad\omega=\Delta\overline{f}\alpha^{2% }\overline{f}\beta\psi,$  (36) 
in terms of $\overline{f}\colon\mathbb{R}\times N\to\mathbb{R}$ and the Poisson bracket $\{\cdot,\cdot\}$ on $N$. On $N=\mathbb{R}^{2}$ with $\psi(x,y)=y$, we obtain the standard $\beta$plane approximation (33).
Proof.
Write $u\in T_{\text{id}}G$ as $u=(S_{\theta}f,c)$ where $f=\overline{f}\circ\pi$ for some $\overline{f}\colon N\to\mathbb{R}$ and $c\in\mathbb{R}$. It is sufficient to compute the inner product of the Euler–Arnold equation with an arbitrary $v=(S_{\theta}g,d)$, which takes the form $\langle\!\langle\dot{u},v\rangle\!\rangle+\langle\!\langle u,\operatorname{ad}% _{u}v\rangle\!\rangle=0$. Here we have
$\operatorname{ad}_{u}v=(\operatorname{ad}_{S_{\theta}f}S_{\theta}g,b(S_{\theta% }f,S_{\theta}g))=\left(S_{\theta}\{f,g\},\int_{M}pS_{\theta}\{f,g\}(q)\right),$ 
in terms of the contact bracket (5) on $M$. However we note that $\{f,g\}=\{\overline{f},\overline{g}\}\circ\pi$ for $E$invariant functions in terms of the quotient Poisson bracket on $N$. In addition since $p$, $q$, $f$, and $g$ are all $E$invariant, we have
$\begin{align}&\int_{M}pS_{\theta}\{f,g\}(q)\,d\mu=\int_{M}p\{\{f,g\},q\}\,d\mu=L\int_{N} \overline{p}\{\{\overline{f},\overline{g}\},\overline{q}\}\,d\nu\\ &\quad=L\int_{N}\{\overline{p},\overline{q}\}\{\overline{f},\overline{g}\}\, d\nu=L\int_{N}\overline{\psi}\{\overline{f},\overline{g}\}\,d\nu=L\int_{N} \overline{g}\{\overline{f},\overline{\psi}\}\,d\nu,\end{align}$ 
where $\nu$ is the volume form on $N$ and $L$ is the length of the Reeb field orbit.
From here we easily compute
0  $\displaystyle=\langle\!\langle u_{t},v\rangle\!\rangle+\langle\!\langle u,% \operatorname{ad}_{u}v\rangle\!\rangle$  
$\displaystyle=\int_{M}g\widetilde{\Delta_{\theta}}f_{t}\,d\mu+c_{t}d\int_{M}% \widetilde{\Delta_{\theta}}f\{f,g\}\,d\mu+L\int_{N}\overline{g}\{\overline{f},% \overline{\psi}\}\,d\nu$  
$\displaystyle=L\int_{N}\overline{g}(\alpha^{2}\overline{f}_{t}\Delta\overline% {f}+\{\overline{f},\alpha^{2}f\Delta f\}+\{\overline{f},\overline{\psi}\})\,d% \nu+c_{t}d.$ 
This is zero for every $g$ and $d$ if and only if $c_{t}=0$ and Eq. (36) holds. $\square$
In general, conservation of the potential vorticity $\omega$ in Eq. (36) implies global existence just as in Corollary 4.3.
4.2 Other Aspects of the Contactomorphism Equation
In this section we will remark on some interesting features of the contactomorphism equation: in particular some special infiniteenergy oneparameter solutions, peakon solutions supported on submanifolds of codimension one (analogous to the standard peakons in the Camassa–Holm equation), and a few conservation laws which are analogous to the first few conserved quantities in the infinite hierarchy in the Camassa–Holm equation.
4.2.1 InfiniteEnergy Solutions
Although we have proved Theorems 3.1 and 3.3 under the assumption that the contact manifold $M$ is compact, the equation (2) makes sense even if $M$ is not compact, as long as the stream function $f$ has compact support or decays sufficiently quickly. The situation we discuss here on $\mathbb{R}^{3}$ does not satisfy these properties, but gives a onedimensional equation that can be studied in some detail, and helps illustrate the similarities between Eq. (2) and the Camassa–Holm equation.
We work with the standard Darboux contact form $\theta=dzy\,dx$ on $\mathbb{R}^{3}$, with Reeb field $E=\frac{\partial}{\partial z}$. A natural Riemannian metric in this case is given by
$ds^{2}=(dzy\,dx)^{2}+dx^{2}+dy^{2},$ 
since in this case the metric is associated, as discussed in Example 2.4. Consider a stream function $f$ of the form $f(t,x,y,z)=zg(t,y)$ for some function $g$; then $m(t,x,y,z)=z[g(t,y)g_{yy}(t,y)]$, and $u=zg_{y}\,\partial_{x}+yg_{y}\,\partial_{y}+z(gyg_{y})\,\partial_{z}$. We can check that the Lie subalgebra consisting of such vector fields generates a totally geodesic submanifold, or simply verify that stream functions of this form give solutions of (2); the equation that $g(t,y)$ must satisfy ends up being
$g_{t}g_{tyy}+4g^{2}4gg_{yy}=ygg_{yyy}yg_{y}g_{yy}.$  (37) 
The problem is that no such stream function can have finite $H^{1}$ norm on $\mathbb{R}^{3}$, and hence results that one can prove about (37) do not necessarily apply to (2), in much the same way that infiniteenergy solutions of the equations of twodimensional hydrodynamics may blow up in finite time [Childress et al.1989] although finiteenergy solutions cannot. However the simpler onedimensional case can give clues to the behavior of the higherdimensional situation.
Sarria and the second author proved the following theorem [Preston and Sarria2014]. It gives a clue as to the role of the sign of the momentum in blowup, although the results are not directly applicable to our case.
Theorem 4.5.
Define $\phi_{0}(y)=g_{0}(y)g_{0}^{\prime\prime}(y)$, and assume $g_{0}$ is $C^{2}$ and satisfies the decay condition $\phi_{0}(y)=O(1/y^{2})$ as $\lvert y\rvert\to\infty$. Then there is a $T>0$ such that there is a unique solution of (37) with $g(0,y)=g_{0}(y)$, and $y\mapsto g(t,y)$ is $C^{2}$ for each $t$. If $\phi_{0}$ is nonnegative, then so is $g_{0}$, and solutions exist globally in time. On the other hand, if $g_{0}$ is even and negative, then solutions blow up at some time $T$ and $g(t,y)\to\infty$ as $t\nearrow T$ for every $y\in\mathbb{R}$.
Essentially what happens here is that the integral of the momentum $\phi=gg_{yy}$ is not conserved (as it would be in the finiteenergy case).^{5}^{5}Note that the actual momentum is $m(t,x,y,z)=z\phi(t,y)$, so the integral of it over the unbounded $z$ domain is infinite. Instead one can show that $\frac{d}{dt}\int_{\mathbb{R}}\phi(t,y)\,dy\leq 0$. The momentum gets transported by the flow $\gamma$ of the vector field $y\mapsto yg(t,y)$, in the sense that $\phi(t,\gamma(t,y))=\phi_{0}(y)y^{5}\gamma_{y}(t,y)/\gamma(t,y)^{5}$, the analogue of the momentum conservation law (15). Thus if $\phi_{0}(y)$ never changes sign, then neither does $\phi(t,y)$ for any $t>0$. Furthermore we can prove that if $\phi$ never changes sign, we have the global bound
$\lvert g_{y}(t,y)\rvert\leq\lvert g(t,y)\rvert\quad\text{for all }\,\,t\,\,\hbox{and}\,\,y.$  (38) 
If $\phi_{0}$ is nonnegative, then the $L^{1}$ norm of $\phi$ decays in time, and we obtain a global $L^{1}$ bound on $\phi$ which is sufficient to obtain an $L^{\infty}$ bound on $g$ and hence also $g_{y}$, which gives global existence. On the other hand if $\phi$ and hence $g$ are nonpositive and symmetric about the origin initially, they will remain so for all time, and we can compute the bound $g_{t}(t,0)\leq\sqrt{6}g(t,0)^{2}$. This implies blowup of $g(t,0)$ in finite time along with blowup of $g(t,y)$ for all other $y$ as a consequence of the differential inequality (38).
4.2.2 Peakon Solutions
Euler–Arnold equations of the form (2) satisfying conservation laws that can be expressed in the form (15) have weak solutions where the momentum $m$ is supported on some lowerdimensional collection of subsets. For example the Camassa–Holm equation (3) has solutions which take the form $m(t,\alpha)=\sum_{k=1}^{n}p_{k}(t)\delta(\alphaq_{k}(t))$, where the functions $p_{k}(t)$ and $q_{k}(t)$ satisfy a Hamiltonian system. The velocity field $u=(1\partial_{\alpha}^{2})^{1}m$ is continuous and has cusps at each of the points $q_{k}(t)$. Similarly one may consider singular solutions of the ideal Euler equation; in two dimensions the solutions with vorticity concentrated on points is a wellknown model, and in three dimensions one may consider either the equation for vortex filaments (that is, vorticity concentrated on curves which evolve in space) or for vortex sheets (where vorticity is concentrated on surfaces). See [Khesin2012a] for a general discussion of such solutions in ideal fluids, and [Holm et al.2009] for a discussion in the case of the Camassa–Holm and EPDiff equations. Note that there are subtleties here: for example while peakons in the Camassa–Holm equation are genuine weak solutions due to the rather mild singularity in the onedimensional Green function, point and filament vorticity models are less mathematically rigorous due to the unboundedness of the higherdimensional Green functions; in such cases one may need to apply a renormalization procedure to obtain a closed system.
The general approach is to integrate the conservation law to the form (15) a sum of deltafunction distributions supported on submanifolds of various codimensions. Depending on the codimension, we may end up with a velocity field $u$ that is welldefined even though $m$ is singular, and this velocity field generates a flow $\eta$ along which the supports of $m$ will move. For example in the Camassa–Holm equation the Schwarz kernel of the operator $(1\partial_{\alpha}^{2})^{1}$ is given by $K(\alpha_{1},\alpha_{2})=\tfrac{1}{2}e^{\lvert\alpha_{1}\alpha_{2}\rvert}$ which is bounded, and hence if $m$ is a sum of delta functions, then the velocity field will always be a weak solution in $H^{1}(\mathbb{R})$. More generally one can consider distributions supported on sets of higher codimension, although only when the codimension is one can we expect the Schwartz kernel to be bounded. General singular solutions of this form for the symplectomorphism Euler–Arnold equation [Ebin2012] were studied by [Khesin2012b], particularly in the case of point symplectic vortices.
Heuristically, the conservation law (15) implies that if an initial momentum $m_{0}$ is concentrated on a submanifold $\Gamma_{0}$, then the momentum will be concentrated on a curve $\Gamma(t)$ of submanifolds of the same dimension for all time $t$. The Lagrangian flows $\eta(t)$ will be contactomorphisms for all $t$. Thus for example we could consider the evolution of a Legendrian submanifold (of dimension $n$) or, in case $n=1$ so that $M$ is threedimensional, we could consider the evolution of an overtwisted disc [Etnyre et al.2012].
Here we will just compute a simple example in the situation of Examples 2.4 and 4.1, on the torus $\mathbb{T}^{3}=(\mathbb{R}/2\pi\mathbb{Z})^{3}$. Recall the contact form is $\theta=\sin{z}\,dx+\cos{z}\,dy$, the Reeb field is $E=\sin{z}\,\partial_{x}+\cos{z}\,\partial_{y}$, and the associated metric is the flat Euclidean metric $ds^{2}=dx^{2}+dy^{2}+dz^{2}$. As in Example 2.4 we have
$S_{\theta}f=(f\sin{z}+f_{z}\cos{z})\,\tfrac{\partial}{\partial x}+(f\cos{z}f_% {z}\sin{z})\,\tfrac{\partial}{\partial y}+(f_{y}\sin{z}f_{x}\cos{z})\,\tfrac{% \partial}{\partial z}.\\ $ 
Consider oneparameter stream functions $f$ such that $m=f\Delta f$ is zero except on a twodimensional submanifold. For example if $f=f(z)$, then we solve the equation $f(z)f^{\prime\prime}(z)=0$ for $\pi<z<\pi$, demanding only continuity at $z=\pi=\pi$ (but not differentiability). We obtain $f(z)=\cosh{z}$, for which the velocity field given by ( 4.2.2) is
$u(x,y,z)=(\sin{z}\cosh{z}+\sinh{z}\cos{z})\,\tfrac{\partial}{\partial x}+(% \cosh{z}\cos{z}\sinh{z}\sin{z})\,\tfrac{\partial}{\partial y}.$ 
As $z\searrow\pi$ we obtain $u(x,y,\pi)=\sinh{\pi}\,\tfrac{\partial}{\partial x}\cosh{\pi}\,\tfrac{% \partial}{\partial y}$, while as $z\nearrow\pi$ we have $u(x,y,\pi)=\sinh{\pi}\,\tfrac{\partial}{\partial x}\cosh{\pi}\,\tfrac{% \partial}{\partial y}$. Thus the velocity field has a jump discontinuity across the 2torus $z=\pi=\pi$, where the flow shears horizontally. Since the surface is not moved by the velocity field (i.e, the velocity field is tangent to the singular surface), this is a steady solution of Eq. (2).
This jump discontinuity of tangential components across the singular surface is typical. The basic model is a function satisfying $ff_{zz}=\delta(z)$ on $\mathbb{R}^{3}$ with a singularity at $z=0$, given by $f(x,y,z)=\tfrac{1}{2}e^{\lvert z\rvert}$, which is differentiable in the $x$ and $y$ directions and continuous but not differentiable in the $z$ direction. Suppose $f$ is a solution of $f\Delta f=0$ on the complement of some surface $\Gamma_{0}$, and let $N$ denote a unit normal vector to $\Gamma_{0}$ at a point $p\in\Gamma_{0}$. Let $\{E,P,Q\}$ be an orthonormal frame as in Proposition 2.3, so that $u=S_{\theta}f=fE+E\times\nabla f$ (using the cross product where $E\times P=Q$, $P\times Q=E$, and $Q\times E=P$). Then
$\langle u,N\rangle=f\langle E,N\rangle+\langle N,E\times\nabla f\rangle=f% \langle E,N\rangle+\langle N\times E,\nabla f\rangle.$ 
Since this differentiates $f$ only in the direction $N\times E$ which is tangent to the surface, it is continuous on $\Gamma_{0}$. Thus if we want to interpret the peakon solutions as an evolution equation for a singular surface, we should consider only the evolution of the normal vector field to the surface, which is welldefined.
The only way $u=S_{\theta}f$ is welldefined on the entire manifold is if $u$ never differentiates in the normal direction, which means $E$ would have to be parallel to $N$ everywhere along the singular surface. In other words the tangent plane to the surface would have to be an integral surface of the contact structure, which is of course impossible by the definition of the contact structure. Hence the shear in the velocity field is a characteristic feature of contact geometry.
4.2.3 Conservation Laws
The Camassa–Holm equation (3) is a completely integrable system, which implies that there are sufficiently many conservation laws that one can use them to form actionangle variables in which the flow is linear. The most obvious conservation law is the $H^{1}$ energy given (see e.g., [Lenells2005]) by $C_{1}[m]=\int_{S^{1}}mu\,d\alpha=\int_{S^{1}}u^{2}+u_{\alpha}^{2}\,d\alpha$. Another conservation law (which can be used to generate another compatible Hamiltonian structure) is $C_{2}[m]=\int_{S^{1}}u^{3}+uu_{\alpha}^{2}\,d\alpha$. Others include the quantities $C_{1}[m]=\int_{S^{1}}\sqrt{m}\,d\alpha$ and $C_{0}[m]=\int_{S^{1}}m\,d\alpha$, where the integral of $\sqrt{m}$ is taken over only the subset where $m$ is positive (a similar law works for $\sqrt{m}$ on the subset where $m$ is negative). Some of these laws, in particular $C_{1}$, $C_{0}$, and $C_{1}$, generalize in a very obvious way to our higherdimensional case (2), and we will present those laws here. It is not clear whether the other conservation laws work here or what form they should take, but it would certainly be interesting to obtain a form of complete integrability for Eq. (2); as it is there are very few examples of completely integrable systems in any dimension higher than one; see for example [Khesin et al.2013].
Proposition 4.6.
Suppose $f$ is a solution of the Eq. (2) on a contact manifold of dimension $2n+1$, with an associated Riemannian metric for which $m=f\Delta f$ and for which $E$ is a Killing field. Then the following quantities are constant along any solution:
$C_{0}=\int_{M}m\,d\mu,\quad C_{1,\pm}=\int_{M}m_{\pm}^{r}\,d\mu,\quad\text{ % and }\,\,\,C_{1}=\int_{M}mf\,d\mu,$ 
where $r=\frac{n+1}{n+2}$ and $m_{+}$ and $m_{}$ denote the positive and negative parts of $m$ (i.e., $m_{+}(x)=m(x)$ if $m(x)>0$ and $m_{+}(x)=0$ otherwise).
Proof.
To prove these, we observe that if $u=S_{\theta}f$, then $\operatorname{div}{u}=(n+1)E(f)$ by Proposition 2.3. We can thus write (2) as
$m_{t}+u(m)+\frac{n+2}{n+1}(\operatorname{div}{u})m=0.$  (39) 
Integrating both sides over $M$ we obtain
$\displaystyle\frac{d}{dt}\int_{M}m\,d\mu$  $\displaystyle=\frac{1}{n+1}\int_{M}(\operatorname{div}{u})m\,d\mu$  
$\displaystyle=\int_{M}fE(f)\,d\mu+\int_{M}E(f)\Delta(f)\,d\mu$  
$\displaystyle=\tfrac{1}{2}\int_{M}f^{2}\operatorname{div}{E}\,d\mu\int_{M}% \langle\nabla f,\nabla E(f)\rangle\,d\mu$  
$\displaystyle=\tfrac{1}{2}\int_{M}\lvert\nabla f\rvert^{2}\operatorname{div}{% E}\,d\mu$  
$\displaystyle=0,$ 
since $\operatorname{div}{E}=0$ by Proposition 2.3, and $E$ commutes with the gradient since it preserves the metric (so that $\nabla E(f)=\nabla_{E}\nabla f$).
For the other conservation law, note that on a domain for which $m$ is positive we can write Eq. (39) as
$\partial_{t}(m^{r})+\operatorname{div}{(m^{r}u)}=0,$ 
which immediately leads to the conservation law
$\int_{\Omega(t)}m(t)^{r}\,d\mu=\text{constant},$ 
where $\Omega(t)$ is a domain transported by the flow. But of course by the conservation law (15), the region $\Omega(t)$ on which $m(t)$ is positive is transported by the flow. The same argument leads to conservation of $m_{}$.
Finally, the fact that $C_{1}$ is conserved follows easily from the fact that $C_{1}=\lVert f(t)\rVert^{2}_{H^{1}}=\lVert\widetilde{S_{\theta}}f(t)\rVert^{2}$, which is precisely the energy of the velocity vector of a geodesic (which is always conserved). Alternatively we could derive it directly via integration by parts, as for the other laws. $\square$
Acknowledgements
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