Abstract

Recall that if (Mn,g)(M^n,g) satisfies Ric≥0\mathrm{Ric}\geq 0, then the Li-Yau Differential Harnack Inequality tells us for each nonnegative f:M→R+f:M\to \mathbb{R}^+, with ftf_t its heat flow, that Δftft−∣∇ft∣2ft2+n2t≥0.\frac{Δf_t}{f_t}-\frac{|\nabla f_t|^2}{f_t^2} +\frac{n}{2t}\geq 0. Our main result will be to generalize this to path space PxMP_xM of the manifold. A key point is that instead of considering infinite dimensional gradients and Laplacians on PxMP_xM we will consider a family of finite dimensional gradients and Laplace operators. Namely, for each H01H^1_0-function φ:R+→Rφ:\mathbb{R}^+\to \mathbb{R} we will define the φφ-gradient ∇φF:PxM→TxM\nabla_φF: P_xM\to T_xM and the φφ-Laplacian ΔφF=trφHessF:PxM→RΔ_φF =\text{tr}_φ\mathrm{Hess} F:P_xM\to \mathbb{R}, where HessF\mathrm{Hess} F is the Markovian Hessian and both the gradient and the φφ-trace are induced by nn vector fields naturally associated to φφ under stochastic parallel translation. Now let (Mn,g)(M^n,g) satisfy Ric=0\mathrm{Ric}=0, then for each nonnegative F:PxM→R+F:P_xM\to \mathbb{R}^+ we will show the inequality Ex[ΔφF]Ex[F]−Ex[∇φF]2Ex[F]2+n2∣∣φ∣∣2≥0\frac{E_x [Δ_φF]}{E_x [F]}-\frac{E_x [\nabla_φF]^2}{E_x [F]^2} +\frac{n}{2}|| φ||^2\geq 0 for each φφ, where ExE_x denotes the expectation with respect to the Wiener measure on PxMP_xM. By applying this to the simplest functions on path space, namely cylinder functions of one variable F(γ)≡f(γ(t))F(γ) \equiv f(γ(t)), we will see we recover the classical Li-Yau Harnack inequality exactly. We have similar estimates for Einstein manifolds, with errors depending only on the Einstein constant, as well as for general manifolds, with errors depending on the curvature. Finally, we derive generalizations of Hamilton's Matrix Harnack inequality on path space PxMP_xM. It is our understanding that these estimates are new even on the path space of Rn\mathbb{R}^n.

Explore this paper’s authors, topics and related work.

Building this map preview

BZPEER is loading the nearby papers, people, topics and institutions for this page.

Reviews 0

Write a reviewWrite

No reviews yet.

Discussion 0

Add a commentWrite

No comments yet.