Randomized Kaczmarz is Asympotically Unbiased for Least Squares

I am delighted to share that my paper Randomized Kaczmarz with tail averaging, joint with Gil Goldshlager and Rob Webber, has been posted to arXiv. This paper in particular really benefited from a lot of feedback from discussions with friends, colleagues, and experts, and I’d like to thank everyone who gave us feedback on this paper.

In this post, I want to provide a different and complementary perspective on the results of this paper, and provide some more elementary results and derivations that didn’t make the main paper.

The randomized Kaczmarz (RK) method is an iterative method for solving systems of linear equations Ax = b, whose dimensions will be n\times d throughout this post. Beginning from a trivial initial solution x_0=0, the method works by repeating the following two steps for t = 0,1,2,\ldots:

  1. Randomly sample a row i_t of A with probability

        \[\prob\{ i_t = j\} = \frac{\norm{a_j}^2}{\norm{A}_{\rm F}^2}.\]

    Throughout this post, a_j^\top denotes the jth row of A.
  2. Orthogonally project x_t onto the solution space of the equation a_{i_t}^\top x = b_{i_t}, obtaining x_{t+1} \coloneqq x_t + (b_{i_t} - a_{i_t}^\top x_t)/\norm{a_{i_t}}^2\cdot a_{i_t}.

The main selling point of RK is that it only interacts with the matrix A through row accesses, which makes the method ideal for very large problems where only a few rows of A can fit in memory at a time.

When applied to a consistent system of linear equations (i.e., a system possessing a solution x_\star satisfying Ax_\star = b), RK is geometrically convergent:

(1)   \[\expect\left[ \norm{x_t - x_\star}^2 \right] \le (1 - \kappa_{\rm dem}^{-2})^t \norm{x_\star}^2. \]

Here,

(2)   \[\kappa_{\rm dem} = \frac{\norm{A}_{\rm F}}{\sigma_{\rm min}(A)} = \sqrt{\sum_i \left(\frac{\sigma_i(A)}{\sigma_{\rm min}(A)}\right)^2} \]

is known as the Demmel condition number, and \sigma_i(A) are the singular values of A.1Personally, I find it convenient to write the Demmel condition number as \kappa_{\rm dem} = \kappa \cdot \sqrt{\operatorname{srank}(A)}, where \kappa = \sigma_{\rm max}(A) / \sigma_{\rm min}(A) is the ordinary condition number and \operatorname{srank}(A) = \norm{A}_{\rm F}^2/\sigma_{\rm max}^2(A) is the stable rank of the matrix A. The stable rank is a smooth proxy for the rank or dimensionality of the matrix A. Using this parameter, the rate of convergence is roughly \e^{-t / (\kappa^2 \operatorname{srank}(A))}, so it takes roughly \kappa^2 \operatorname{srank}(A) row accesses to reduce the error by a constant factor. Compare this to gradient descent, which requires \kappa^2 n row accesses. However, for inconsistent problems, RK does not converge at all. Indeed, since each step of RK updates the iterate x_t such that an equation a_{i_t}^\top x = b_{i_t} hold exactly and no solution x_\star satisfies all the equations simultaneously, the RK iterates continue to stochastically fluctuate no matter how long the algorithm is run.

However, while the RK iterates continue to randomly fluctuate when applied to an inconsistent system, their expected value does converge. In fact, it converges to the least-squares solution2If the matrix A is rank-deficient, then we define x_\star to be the minimum-norm least-squares solution x_\star = A^\dagger b, which can be expressed using the Moore–Penrose pseudoinverse {}^\dagger. x_\star to the system, defined as

    \[x_\star = \operatorname{argmin}_{x \in \real^d} \norm{b - Ax}.\]

Put differently, the bias of the RK iterates x_t as estimators to the least-squares solution x_\star converge to zero, and the rate of convergence is geometric. Specifically, we have the following theorem:

Theorem 1 (Exponentially Decreasing Bias): The RK iterates x_t have an exponentially decreasing bias

(3)   \[\norm{\mathbb{E}[x_t] - x_\star}^2 \le (1 - \kappa_{\rm dem}^{-2})^{2t} \norm{x_\star}^2. \]

Observe that the rate of convergence (3) for the bias is twice as fast as the rate of convergence for the error in (1). This factor of two was previously observed by Gower and Richtarik in the context of consistent systems of equations.

The proof of Theorem 1 is straightforward, and we will present it at the bottom of this post. First, we will discuss a couple of implications. First, we develop convergent versions of the RK algorithm using tail averaging. Second, we explore what happens when we implement RK with different sampling probabilities \prob \{i_t = j\}.

Tail Averaging

It may seem like Theorem 1 has little implication for practice. After all, just because the expected value of x_t becomes closer and closer to x_\star, it need not be the case that x_t is close to x. However, we can improve the quality of the approximate solution x_t by averaging.

There are multiple different possible ways we could use averaging. A first idea would be to run RK multiple times, obtaining multiple solutions x^{(1)}_t,\ldots,x^{(m)}_t which could then be averaged together. This approach is inefficient as each solution x_t^{(i)} is computed separately.

A better strategy is tail averaging. Fix a burn-in time t_{\rm b}, chosen so that the bias \norm{\expect[x_{t_{\rm b}}] - x_\star} is small. For each s> t_{\rm b}, x_s is a nearly unbiased approximation to the least-squares solution x_\star. To reduce variance, we can average these estimators together

    \[\overline{x}_t = \frac{x_{t_{\rm b} +1} + x_{t_{\rm b}+2} + \cdots + x_t}{t-t_{\rm b}}.\]

The estimator \overline{x}_t is the tail-averaged randomized Kaczmarz (TARK) estimator. By Theorem 1, we know the TARK estimator has an exponentially small bias:

    \[\norm{\expect[\overline{x}_t] - x_\star} \le (1 - \kappa_{\rm dem}^{-2})^{2(t_{\rm b}+1)} \norm{x_\star}^2.\]

In our paper, we also prove a bound for the mean-square error:

    \[\expect [\norm{\overline{x}_t - x_\star}^2] \le (1-\kappa_{\rm dem}^{-2})^{t_{\rm b}+1} \norm{x_\star}^2 + \frac{2\kappa_{\rm dem}^4}{t-t_{\rm b}} \frac{\norm{b-Ax_\star}^2}{\norm{A}_{\rm F}^2}.\]

We see that the rate of convergence is geometric in the burn-in time t_{\rm b} and occurs at an algebraic, Monte Carlo, rate in the final time t. While the Monte Carlo rate of convergence may be unappealing, it is known that this rate of convergence is optimal for any method that accesses row–entry pairs (a_i,b_i); see our paper for a new derivation of this fact.

Tail averaging can be an effective method for squeezing a bit more accuracy out of the RK method for least-squares problems. The figure below shows the error of different RK methods applied to a random least-squares problem, including plain RK, RK with thread averaging (RKA), and RK with underrelaxation (RKU);3The number of threads is set to 10, and the underrelaxation parameter is 1/\sqrt{t}. We found this underrelaxation parameter to lead to a smaller error than the other popular underrelaxation parameter schedule 1/t. see the paper’s Github for code. For this problem, tail-averaged randomized Kaczmarz achieves the lowest error of all of the methods considered, being 6× smaller than RKA, 22× smaller than RK, and 10⁶× smaller than RKU.

Error versus iteration for different randomized Kaczmarz methods. Tail-averaged randomized Kaczmarz shows the lowest error

What Least-Squares Solution Are We Converging To?

A second implication of Theorem 1 comes from reanalyzing the RK algorithm if we change the sampling probabilities. Recall that the standard RK algorithm draws random row indices i_t using squared row norm sampling:

    \[\prob \{ i_t = j \} = \frac{\norm{a_j}^2}{\norm{A}_{\rm F}^2} \eqqcolon p^{\rm RK}_j.\]

We have notated the RK sampling probability for row j as p_j^{\rm RK}.

Using the standard RK sampling procedure can sometimes be difficult. To implement it directly, we must make a full pass through the matrix to compute the sampling probabilities.4If we have an upper bound on the squared row norms, there is an alternative procedure based on rejection sampling that avoids this precomputation step. It can be much more convenient to sample rows i_t uniformly at random \prob \{ i_t = j \} = 1/n.

To do the following analysis in generality, consider performing RK using general sampling probabilities p_j:

    \[\prob \{i_t = j\} = p_j.\]

What happens to the bias of the RK iterates then?

Define a diagonal matrix

    \[D \coloneqq \diag\left( \sqrt{\frac{p_j}{p_j^{\rm RK}}} : j =1,\ldots,n\right).\]

One can check that the RK algorithm with non-standard sampling probabilities \{p_j\} is equivalent to the standard RK algorithm run on the diagonally reweighted least-squares problem

    \[x_{\rm weighted} = \argmin_{x\in\real^d} \norm{Db-(DA)x}.\]

In particular, applying TARK with uniform sampling probabilities, the tail-averaged iterates \overline{x}_t will converge to the weighted least-squares problem x_{\rm weighted} rather than the original least-squares solution x_\star.

I find this very interesting. In the standard RK method, the squared row norm sampling distribution is chosen to ensure rapid convergence of the RK iterates to the solution of a consistent system of linear equations. However, for a consistent system, the RK method will always converge to the same solution no matter what row sampling strategy is chosen (as long as every non-zero row has a positive probability of being picked). In the least-squares context, however, the conclusion is very different: the choice of row sampling distribution not only affects the rate of convergence, but also which solution is being converged to!

As the plot below demonstrates, the original least-squares solution and re-weighted least-squares solution can sometimes be quite different from each other. This plot shows the results of fitting a function with many kinks (show as a black dashed curve) using a polynomial function p(u) = \sum_{j=0}^{10} x_j u^j[mfn}Note that, for this experiment we represent the polynomial p(u) = \sum_{i=0}^{10} x_j u^j using its monomial coefficients x_j, which has issues with numerical stability. It’s better to use a representation using Chebyshev polynomials. We use this example only to illustrate the difference between the weighted and original least-squares solution.[/mfn} at 10000 equispaced points. We compare the unweighted least-squares solution (orange solid curve) to the weighted least-squares solution using uniform RK weights p_j = 1/n (blue dash-dotted curve). These two curves differ meaningfully, with the weighted least-squares solution having higher error at the ends of the interval but more accuracy in the middle. These differences can be explained looking at the weights (diagonal entries of D, grey dotted curve), which are lower at the ends of the interval than in the center.

Weighted and un-weighted least-squares solution to polynomial regression problem. (Tail averaged) randomized Kaczmarz method with uniform sampling converges to the weighted least-squares solution, which is more accurate on the middle of the interval (where the weights are high) than the edges of the interval (where the weights are smaller)

Does this diagonal rescaling issue matter? Sometimes not. In many applications, the weighted and un-weighted least squares solutions will both be fine. Indeed, in the above example, neither the weighted nor un-weighted solutions are the “right” one; the weighted solution is more accurate in the interior of the domain and less accurate at the boundary. However, sometimes getting the true least-squares solution matters, or the amount of reweighting done by uniform sampling is too aggressive for a problem. In these cases, using the classical RK sampling probabilities may be necessary. Fortunately, rejection sampling can often be used to perform squared row norm sampling; see this blog post of mine for details.

Proof of Theorem 1

Let us now prove Theorem 1, the asymptotic unbiasedness of randomized Kaczmarz. We will assume throughout that A is full-rank; the rank-deficient case is similar but requires a bit more care.

Begin by rewriting the update rule in the following way

    \[x_{t+1} = \left( I - \frac{a_{i_t}^{\vphantom{\top}}a_{i_t}^\top}{\norm{a_{i_t}}^2} \right)x_t + \frac{b_{i_t}a_{i_t}}{\norm{a_{i_t}}^2}.\]

Now, letting \expect_{i_t} denote the average over the random index i_t, we compute

    \begin{align*}\expect_{i_t}[x_{t+1}] &= \sum_{j=1}^n \left[\left( I - \frac{a_j^{\vphantom{\top}} a_j^\top}{\norm{a_j}^2} \right)x_t + \frac{b_ja_j}{\norm{a_j}^2}\right] \prob\{i_t=j\}\\ &=\sum_{j=1}^n \left[\left( \frac{\norm{a_j}^2}{\norm{A}_{\rm F}^2}I - \frac{a_j^{\vphantom{\top}} a_j^\top}{\norm{A}_{\rm F}^2} \right)x_t + \frac{b_ja_j}{\norm{A}_{\rm F}^2}\right].\end{align*}

We can evaluate the sums \sum_{j=1}^n a_j^{\vphantom{\top}}a_j^\top = A^\top A and \sum_{j=1}^n b_j a_j = A^\top b directly. Therefore, we obtain

    \[\expect_{i_t}[x_{t+1}] = \left( I - \frac{A^\top A}{\norm{A}_{\rm F}^2}\right) x_t + \frac{A^\top b}{\norm{A}_{\rm F}^2}.\]

Thus, taking the (total) expectation of both sides, we get

    \[\expect[x_{t+1}] = \left( I - \frac{A^\top A}{\norm{A}_{\rm F}^2}\right) \expect[x_t] + \frac{A^\top b}{\norm{A}_{\rm F}^2}.\]

Iterating this equation and using the initial condition x_0 = 0, we obtain

(4)   \[\expect[x_t] = \left[\sum_{i=0}^{t-1} \left( I - \frac{A^\top A}{\norm{A}_{\rm F}^2}\right)^i \right]\cdot\frac{A^\top b}{\norm{A}_{\rm F}^2}.\]


The equation (4) expresses the expected RK iterate \expect[x_t] using a matrix geometric series. Recall that the infinite geometric series with a scalar ratio |y|<1 satisfies the formula

    \[\sum_{i=0}^\infty y^i = (1-y)^{-1}.\]

Substituting x=1-y, we get

    \[\sum_{i=0}^\infty (1-x)^i = x^{-1}\]

for any 0 < x < 2. With a little effort, one can check that the same formula

    \[\sum_{i=0}^\infty (I-X)^i = X^{-1}\]

for a square matrix X satisfying 0 < \sigma_{\rm min}(X) \le \norm{X} < 2. These conditions hold for the matrix X = A^\top A / \norm{A}_{\rm F}^2 since A is full-rank, yielding

(5)   \[\left(\frac{A^\top A}{\norm{A}_{\rm F}^2}\right)^{-1} = \sum_{i=0}^\infty \left( I - \frac{A^\top A}{\norm{A}_{\rm F}^2}\right)^i. \]

In anticipation of plugging this result into (4), we can break the infinite sum on the right-hand side into two pieces:

(6)   \[\left(\frac{A^\top A}{\norm{A}_{\rm F}^2}\right)^{-1} = \sum_{i=0}^{t-1} \left( I - \frac{A^\top A}{\norm{A}_{\rm F}^2}\right)^i + \sum_{i=t}^\infty \left( I - \frac{A^\top A}{\norm{A}_{\rm F}^2}\right)^i.\]

We are at the home stretch. Plugging (6) into (4) and using the normal equations x_\star = (A^\top A)^{-1} A^\top b, we obtain

    \[\expect[x_t] = x_\star - \left[\sum_{i=t}^\infty \left( I - \frac{A^\top A}{\norm{A}_{\rm F}^2}\right)^i \right]\cdot\frac{A^\top b}{\norm{A}_{\rm F}^2}.\]

Rearrange to obtain

    \[\expect[x_t] - x_\star = - \left(I - \frac{A^\top A}{\norm{A}_{\rm F}^2}\right)^t \left[\sum_{i=0}^\infty \left( I - \frac{A^\top A}{\norm{A}_{\rm F}^2}\right)^i \right]\cdot\frac{A^\top b}{\norm{A}_{\rm F}^2}.\]

Now apply (5) and the normal equations again to obtain

    \[\expect[x_t] - x_\star = - \left(I - \frac{A^\top A}{\norm{A}_{\rm F}^2}\right)^t x_\star.\]

Take norms and use the submultiplicative property of the spectral norm to obtain

(7)   \[\norm{\expect[x_t] - x_\star}^2 \le \norm{I - \frac{A^\top A}{\norm{A}_{\rm F}^2}}^{2t} \norm{x}_\star^2. \]

To complete the proof we must evaluate the norm of the matrix I - A^\top A / \norm{A}_{\rm F}^2. Let A = U \Sigma V^\top be a (thin) singular value decomposition, where \Sigma = \diag(\sigma_{\rm max}(A),\ldots,\sigma_{\rm min}(A)). Then

    \[I - \frac{A^\top A}{\norm{A}_{\rm F}^2} = I - V \cdot\frac{\Sigma^2}{\norm{A}_{\rm F}^2} \cdot V^\top = V \left( I - \frac{\Sigma^2}{\norm{A}_{\rm F}^2}\right)V^\top.\]

We recognize this as a matrix whose eigenvectors are V and whose eigenvalues are the diagonal entries of the matrix

    \[I - \Sigma^2/\norm{A}_{\rm F}^2 = \diag(1 - \sigma^2_{\rm max}(A)/\norm{A}_{\rm F}^2,\ldots,1-\sigma_{\rm min}^2(A)/\norm{A}_{\rm F}^2).\]

All eigenvalues are nonnegative and the largest eigenvalue is 1 - \sigma_{\rm min}^2(A)/\norm{A}_{\rm F}^2 = 1 - \kappa_{\rm dem}^{-2}. We have invoked the definition of the Demmel condition number (2). Therefore, plugging into (7), we obtain

    \[\norm{\expect[x_t] - x_\star}^2 \le \left(1-\kappa_{\rm dem}^{-2}\right)^{2t} \norm{x}_\star^2,\]

as promised.

Note to Self: Sketch-and-Solve with a Gaussian Embedding

In the comments to my post Does Sketching Work?, I was asked a very interesting question, which I will paraphrase as follows:

Is the sketch-and-solve least-squares solution \hat{x} = \operatorname*{argmin}_{\hat{x}} \norm{(SA)\hat{x} - Sb} an unbiased estimate of the true least squares solution of x = \operatorname*{argmin}_x \norm{Ax - b}?

In this post, I will answer this question for the special case in which S is a Gaussian sketch, and I will also compute the expected least-squares residual \expect \norm{A\hat{x}-b}^2. Throughout this post, I will assume knowledge of sketching; see my previous two posts for a refresher if needed. For this post, A will have dimensions n\times d and S will have dimensions \ell\times n, and these parameters are related n\ge \ell \ge d.

I thought I knew the answer to this question—that sketch-and-solve suffers from inversion bias. Indeed, the fact I remembered is that

(1)   \[\expect\Big[\big((SA)^\top (SA)\big)^{-1}\Big] \ne \big(A^\top A\big)^{-1}\]

for the sketching matrices S in common use. The issue of the inversion bias (1) is discussed in this paper.

However, the inversion bias (1) does not imply that sketch-and-solve is biased. In fact, for a Gaussian sketch1Note that, typically, we use a sketch S where the variance of the entries is 1/d. The sketch-and-solve solution (SA)^\dagger (Sb) does not change under a scaling of the matrix S. Thus, we are free to take the entries to have variance one.

(2)   \[S \in \real^{\ell\times n} \quad \text{with } S_{ij} \sim \text{Normal}(0,1) \text{ iid},\]

sketch-and-solve is unbiased.

Theorem (Gaussian sketch-and-solve is unbiased). Let S be a Gaussian sketch (2) and let A \in \real^{n\times d} be a full column-rank matrix. Then

(3)   \[\expect[(SA)^\dagger(Sb)] = A^\dagger b. \]

That is, the sketch-and-solve solution (SA)^\dagger(Sb) is an unbiased estimate for the least-squares solution A^\dagger b.

Here, {}^\dagger is the Moore–Penrose pseudoinverse, which effectuates the least-squares solution:

    \[A^\dagger b = \operatorname*{argmin}_{x\in\real^d} \norm{Ax - b}.\]

In particular, by the normal equations, we have the relation

(4)   \[A^\dagger = (A^\top A)^{-1} A^\top,\]

valid for any matrix A with full column-rank.

Let us prove this theorem. The Gaussian sketch (1) is orthogonally invariant: that is, V^\top SU has the same distribution as S for any orthogonal matrices U and V. Thus, we are free to reparametrize. Let

    \[A = U\twobyone{\Sigma}{0}V^\top\]

be a (full) singular value decomposition of A. Make the changes of variables

    \[A \mapsto U^\top A V, \quad S \mapsto V^\top SU, \quad b \mapsto U^\top b.\]

After this change of variables, S still has the same distribution (2) and

    \[A = \twobyone{\Sigma}{0}.\]

Partition the reparametrized b and S conformally with A:

    \[b = \twobyone{b_1}{b_2}, \quad S = \onebytwo{S_1}{S_2}.\]

Under this change of variables, the least-squares solution is

(5)   \[A^\dagger b = \Sigma^{-1}b_1.\]

Now, we are ready to prove the claim (3). Observe that SA = S_1\Sigma. Begin by using the normal equations (4) to write out the sketch-and-solve solution

    \[(SA)^\dagger (Sb) = [(SA)^\top (SA)]^{-1}(SA)^\top (Sb).\]

Observe that SA = S_1\Sigma. Thus,

    \[(SA)^\dagger (Sb) = [\Sigma S_1^\top S_1\Sigma]^{-1}\Sigma S_1^\top \onebytwo{S_1}{S_2}\twobyone{b_1}{b_2}.\]

Simplify to obtain

    \[(SA)^\dagger (Sb) = \Sigma^{-1}(S_1^\top S_1)^{-1} S_1^\top (S_1b_1 + S_2 b_2).\]

Using the normal equations (4) and the solution formula (5), we obtain

(6)   \[(SA)^\dagger (Sb) = \Sigma^{-1}b_1 + \Sigma^{-1} S_1^\dagger S_2b_2 = A^\dagger b + \Sigma^{-1} S_1^\dagger S_2b_2. \]

By the definition (2) of S, S_1 and S_2 are independent and \expect[S_2] = 0. Thus, taking expectations, we obtain

    \[\expect[(SA)^\dagger (Sb)] = A^\dagger b + \Sigma^{-1} \expect[S_1^\dagger] \expect[S_2]b_2 = A^\dagger b.\]

The desired claim (3) is proven.

Note that the solution formula (6) holds for any sketching matrix S. We only use Gaussianity at the last step, where we invoke three properties (1) S is mean zero; (2) S is orthogonally invariant; and (3) conditional on the first d columns of S, the last n-d columns of S are mean-zero.

The Least-Squares Residual for Gaussian Sketch-and-Solve

The solution formula (6) can be used to understand other properties of the Gaussian sketch-and-solve solution. In this section, we use (6) to understand the expected squared residual norm

    \[\expect \norm{A\hat{x} - b}^2,\]

where \hat{x} = (SA)^\dagger (Sb) is the sketch-and-solve solution. We write the expected residual norm as

    \[\expect\norm{A\hat{x} - b}^2 = \expect\norm{\twobyone{b_1 + S_1^\dagger S_2b_2}{0} - \twobyone{b_1}{b_2}}^2 = \norm{b_2}^2 + \expect\norm{S_1^\dagger S_2b_2}^2.\]

Now, use the Gaussian–inverse Gaussian matrix product formula to compute the expectation, obtaining

    \[\expect\norm{A\hat{x} - b}^2 = \left(1+\frac{d}{\ell-d-1}\right)\norm{b_2}^2.\]

Finally, we recognize \norm{b_2} is the optimal least-squares residual \min_x \norm{Ax - b}. Thus, we have shown

    \[\expect\norm{A\hat{x} - b}^2 = \left(1+\frac{d}{\ell-d-1}\right)\min_{x\in\real^d} \norm{Ax-b}^2.\]

Note that this is an exact formula for the expected squared residual for the sketch-and-solve solution! Thus, the sketch-and-solve solution has an expected squared residual that factor 1 + d/(\ell-d-1) larger than the optimal value. In particular,

    \[\expect\norm{A\hat{x} - b}^2 = \left(1+\varepsilon\right)\min_{x\in\real^d} \norm{Ax-b}^2 \quad \text{when } \ell = \frac{d}{\varepsilon} + d + 1.\]

Remark (Existing literature): When I originally wrote this post, I had not seen these results anywhere in the literature. Thanks to Michał Dereziński, who provided me with the following references: the following lecture notes of Mert Pilanci, equation 1 in this recent paper of Michał’s, and this recent survey by Michał and Michael Mahoney. I find it striking that these basic and beautiful results appear to only have been explicitly recorded very recently. Very big thanks also to Rob Webber for providing help in preparing this post.

Update (11/21/24): After this post was initially released, Mert Pilanci provided me with an earlier reference (2020); see also this paper for extensions. He also mentions an even earlier paper (2017) that does similar calculations in a statistical setting, but does not obtain exactly these formulas. See also this paper for exact and asymptomatically exact formulas for sketch-and-solve in the statistical setting.

Note to Self: Hanson–Wright and Trace Estimation with Random Vectors on the Sphere

Tyler Chen has just released an excellent monograph on the Lanczos method, one of the most powerful algorithms for extracting information from a symmetric matrix A. I would definitely recommend checking it out.

One of the subjects touched on by this book is stochastic trace estimation, a topic I’ve written about several times before on this blog. In his book, Tyler uses stochastic trace estimates based on random vectors on the sphere (a great choice), and he provides a simple, but often pessimistic, mathematical analysis of this approach. To complement Tyler’s amazing book, I felt it was a good opportunity to share a sharper analysis that I came up with using a more sophisticated argument. I would not be surprised if this argument appears elsewhere in the literature, but I am not aware of a source.

Let x,x_1,\ldots,x_m be random vectors in \real^n drawn uniformly at random from the sphere of radius \sqrt{n},1Informally, we define the uniform distribution on the sphere to be such that the probability that x belongs to a set U is the ratio of the (hyper-)surface area of U to the (hyper-)surface area of the full sphere. Formally, the uniform distribution on the sphere can be defined multiple ways. First, treating the sphere as a subset of \real^n, we can define the uniform distribution as the (n-1)-dimensional Hausdorff measure, normalized so that the sphere has unit measure. Second, observe that the sphere is acted upon in a natural way by the group of orthogonal matrices. The uniform distribution is the unique probability measure which is invariant to this group action. let A be a real symmetric matrix, and define the quadratic form

    \[q \coloneqq x^\top Ax\]

and the Girard–Hutchinson trace estimator

    \[\hat{\tr}\coloneqq \frac{1}{m}\sum_{i=1}^m x_i^\top Ax_i.\]

Both q and \hat{\tr} are unbiased estimates for the trace of A, \expect[q] = \expect[\hat{\tr}] = \tr A. The goal of this post will be to bound the probability of these quantities being much smaller or larger than the trace of A.

Hanson–Wright on the Sphere

Observe that \hat{\tr} is an average of m independent copies of the random variable q. Therefore, we will begin our analysis with the quadratic form q and discuss the Girard–Hutchinson estimate \hat{\tr} at the end of the post.

Centering

Begin by introducing the centered matrix

    \[\overline{A} = A - \frac{\tr A}{n}I.\]

The transformation A\mapsto\overline{A} has the effect of shifting A’s eigenvalues to have mean zero. Consequently, since the trace is the sum of the eigenvalues, \overline{A} has trace zero.

Now, rewrite q in terms of the centered matrix \overline{A}:

    \[q = x^\top A x = x^\top \overline{A} x + \frac{\tr A}{n} \cdot x^\top I x = x^\top \overline{A} x + \tr A.\]

In the final equality, we use the fact that x is on the sphere of radius \sqrt{n} so that x^\top I x = \norm{x}^2 = n. Rearranging, we see that the error \overline{q}\coloneqq q-\tr A satisfies

    \[\overline{q} = q-\tr A = x^\top \overline{A}x.\]

We have shown that the error \overline{q} depends only on the centered matrix \overline{A} rather than the original matrix A. This observation is at the root of the reason that quadratic forms with vectors on the sphere have smaller tail probabilities than other distributions like the Gaussian distribution. Indeed, \overline{A} is smaller than A when measured using the Frobenius norm \norm{\overline A}_{\rm F} \le \norm{A}_{\rm F}, and the spectral norm is never much larger \norm{\overline{A}} \le 2\norm{A}. These observations will be important later.

Laplace Transform Method and Comparison to Standard Gaussian Vectors

To derive exponential concentration inequalities, we make use of the Laplace transform method. For a random variable z, define the cumulant generating function (cgf)

    \[\xi_z(\theta) = \log (\expect [\exp(\theta z)]).\]

Bounds on the cgf immediately yield bounds on the random variable taking large values, so it will behoove us to estimate this quantity for \overline{q}.

To estimate the cgf of \overline{q}, we will make use of a comparison between Gaussian vectors and random vectors on the sphere. Recall that a standard Gaussian vector g is a vector with independent standard Gaussian entries. Standard Gaussian random vectors are spherically symmetric, meaning they can be written in the form g = a\cdot x, where x is a uniform random vector on the sphere and a is a scaling factor.2Concretely, a\sqrt{n} is a \chi random variable with n degrees of freedom. The scaling factor a is independent of x and, in this case, satisfies \expect[a^2] = 1.3Indeed, the expected squared length of a standard Gaussian random vector is \expect[\norm{g}^2] = \sum_{i=1}^n \expect[g_i^2] = n. But also, \expect[\norm{g}^2] = \expect[a^2] \cdot \expect[\norm{x}^2] = \expect[a^2] \cdot n. Therefore, \expect[a^2]=1.

Using this relationship, the error \overline{q} can be connected to the standard Gaussian random vector g as follows

    \[g^\top \overline{A} g = a^2 \cdot x^\top \overline{A} x = a^2 \cdot \overline{q}.\]

Intuitively, we might expect that multiplying the random error \overline{q} by a scaling factor of mean one should only have the effect of increasing the variability of \overline{q} and thus increasing its probability of taking large values. Based on this intuition, we might conjecture that the cgfs are related

    \[\xi_{\overline{q}}(\theta) \le \xi_{g^\top A g}(\theta) \quad \text{for all } \theta \in \real.\]

Indeed, this conjecture is true.

Proposition (Scaling hurts). Let z be a random variable and let b be a random variable with expectation 1, independent of z. Then

    \[\xi_{z}(\theta) \le \xi_{bz}(\theta) \quad \text{for all } \theta \in \real.\]

To prove this result, let \expect_b and \expect_z denote expectations take over the randomness in b and z separately. The total expectation is \expect[\cdot] = \expect_z[\expect_b[\cdot ]]. Begin with the right-hand side and invoke Jensen’s inequality over b:

    \[\xi_{bz}(\theta) = \xi_z(\theta) = \log (\expect_z [\expect_b [\exp(\theta bz)]]) \ge \log (\expect_z [\exp(\theta \expect_b[b]z)]) = \xi_z(\theta).\]

In the last line, we use the hypothesis \expect[b] = 1 and the definition of the cgf.

Having established this proposition, we conclude that \xi_{\overline{q}}(\theta) \le \xi_{g^\top \overline{A} g}(\theta) for all \theta.

Completing the Analysis

Finally, invoking a standard bound for the cgf of g^\top \overline{A}g for a trace-zero matrix \overline{A}, we obtain

    \[\xi_{\overline{q}}(\theta) \le \xi_{g^\top \overline{A} g}(\theta) \le \frac{\theta^2 \norm{\overline{A}}_{\rm F}^2}{1 - 2\theta \norm{\overline{A}}}.\]

A cgf bound of this form immediately yields the following tail bound (see BoucheronLugosi, and Massart’s Concentration Inequalities page 29 and Exercise 2.8):

    \[\prob \{ x^\top A x - \tr(A) \ge t \} \le \exp \left( - \frac{t^2/2}{2 \norm{\overline{A}}_{\rm F}^2 + 2 \overline{\norm{\overline{A}}t}} \right).\]

One can also control the lower tail event x^\top A x - \tr(A) \le -t by instantiating this result with -A. Union bounding over the upper and lower tails gives the symmetric bound

    \[\prob \{ |x^\top A x - \tr(A)| \ge t \} \le 2\exp \left( - \frac{t^2/2}{2 \norm{\overline{A}}_{\rm F}^2 + 2 \overline{\norm{\overline{A}}t}} \right).\]

Is This Bound Good?

Tail bounds for quadratic forms such as x^\top A x or g^\top A g are known as Hanson–Wright inequalities. For vectors on the sphere, our bound shows the tail probabilities decay like \exp(-O(t^2/\norm{\overline{A}_{\rm F}}^2)) for small t > 0 and \exp(-O(t/\norm{\overline{A}})) for large t>0. This pattern of results “subgaussian scaling for small t, subexponential scaling for large t” is typical for Hanson–Wright inequalities.

The Hanson–Wright inequalities for vectors on the sphere exhibit faster decay rate than for standard Gaussian vectors. Indeed, a standard Gaussian random vector g obeys a Hanson–Wright inequality of the form

    \[\prob \{ g^\top A g - \tr A \ge t \} \le \exp \left( -\frac{t^2/2}{C\norm{A}_{\rm F}^2 + c t \norm{A}}\right)\]

for positive constants C,c > 0. For vectors on the sphere, \norm{A}_{\rm F}^2 and \norm{A} have been replaced by \norm{\overline{A}}_{\rm F}^2 and \norm{\overline{A}} which are always smaller (and sometimes much smaller). The smaller tail probabilities for x^\top A x versus g^\top A g is a real phenomenon, not an artifact of the mathematical analysis.

As another way to evaluate the quality of these bounds, recall that a Gaussian random variable with mean zero and variance v has tail probabilities roughly of size \exp(-t^2/2v). For small t, our Hanson–Wright inequality for vectors on the sphere has the same form with v = 2\norm{\overline{A}}_{\rm F}^2. The true variance of q = x^\top A x is

    \[\Var(q) = \frac{n}{n+2} \cdot 2\norm{\overline{A}}_{\rm F}^2,\]

which is close to v = 2\norm{\overline{A}}_{\rm F}^2 for large n. (See this post of mine for a derivation of the variance formula.) Thus, even up to the constants, the Hanson–Wright inequality we’ve derived for random vectors on the sphere is nearly as good as one could possibly hope (at least for small t).

Girard–Hutchinson Estimator on the Sphere

Using our results for one quadratic form, tail bounds for the Girard–Hutchinson estimator \overline{\tr} = m^{-1} \sum_{i=1}^m x_i^\top A x_i easily follow. Indeed, the cgf is additive for independent random variables and satisfies the identity \xi_{cz}(\theta) = \xi_z(c\theta) for constant $c, so

    \[\xi_{\overline{\tr}}(\theta) = \sum_{i=1}^m \xi_{x_i^\top Ax_i}(\theta/m) \le m \cdot \frac{(\theta/m)^2 \norm{\overline{A}}_{\rm F}^2}{1 - 2(\theta/m)\norm{\overline{A}}}.\]

This cgf bound leads to tail bounds

    \begin{align*}\prob \{ \overline{\tr} - \tr(A) \ge t \} &\le \exp \left( - \frac{t^2/2}{2m \norm{\overline{A}}_{\rm F}^2 + 2m \overline{\norm{\overline{A}}t}} \right), \\\prob \{ |\overline{\tr} - \tr(A)| \ge t \} &\le 2\exp \left( - \frac{t^2/2}{2m \norm{\overline{A}}_{\rm F}^2 + 2m \overline{\norm{\overline{A}}t}} \right).\end{align*}

Rejection Sampling

I am delighted to share that my paper Embrace rejection: Kernel matrix approximation with randomly pivoted Cholesky has been released on arXiv, joint with Joel Tropp and Rob Webber.

On the occasion of this release, I want to talk about rejection sampling, one of the most powerful ideas in probabilistic computing. My goal is to provide an accessible and general introduction to this technique, with a more “applied math” rather than statistical perspective. I will conclude with some discussion of how we use it in our paper.

Motivating Application: Randomized Kaczmarz

Consider the task of solving a linear system of equations Ax = b, where A \in \real^{n\times d} is a matrix and b \in \real^n is a vector. For simplicity, we assume that this system is consistent (i.e., there exists a solution x_\star such that Ax_\star = b). The randomized Kaczmarz algorithm is a mathematically elegant algorithm for solving this problem, due to Strohmer and Vershynin. Beginning with initial solution x \gets 0, randomized Kaczmarz repeatedly performs the following steps:

  1. Sample. Generate a random row index I according to the probability distribution \prob \{I = i\} = \norm{a_i}^2 / \norm{A}_{\rm F}^2. Here, and going forward, a_i^\top denotes the ith row of A and \norm{\cdot}_{\rm F} is the Frobenius norm.
  2. Update. Set x \gets x + (b_I - a_I^\top x)\cdot a_I / \norm{a_I}^2.

Convergence theory of the randomized Kaczmarz iteration is very well-studied; see, e.g., section 4.1 of this survey for an introduction.

For this post, we will consider a more basic question: How can we perform the sampling step 1? If n and d are not very large, this is an easy problem: Simply sweep through all the rows a_i and compute their norms \norm{a_i}^2. Then, sampling can be done using any algorithm for sampling from a weighted list of items. But what if n is very large? Suppose, even, that it is computationally expensive to read through the matrix, even once, to compute the row norms. What can we do now?

Here is one solution is using rejection sampling. Suppose that we know a bound on the row norms of A:

(1)   \[\norm{a_i}^2 \le B \quad \text{for each } i = 1,\ldots,n.\]

For instance, if the entries of A take values in the range [-1,1], then (1) holds with B = d. To sample a row i with probability \norm{a_i}^2/\norm{A}_{\rm F}^2, we perform the following the rejection sampling procedure:

  1. Propose. Draw a random row index 1\le J\le n uniformly at random (i.e., J is equally likely to be any row index between 1 and n.)
  2. Accept/reject. Make a random choice: With probability p_J = \norm{a_J}^2/B, accept and set I\gets J. With the remaining probability 1-p_J, reject and return to step 1.

Why does this procedure work? As an intuitive explanation, notice that each row i is equally likely to be proposed and has probability proportional to \norm{a_i}^2 of being accepted. Therefore, under this procedure, each row i has probability proportional to \norm{a_i}^2 of being selected, just as desired for randomized Kaczmarz. If this intuitive justification is unsatisfying, we’ll have a formal derivation of correctness below (in a more general context).

I find rejection sampling to be super neat. In this case, it allows us to use simple ingredients (uniform row sampling and an upper bound on the row norms) to accomplish a more complicated task (sampling according to the squared row norms). We can sample from an interesting probability distribution (the squared row norm distribution) by thinning out samples from a simple distribution. This is a powerful idea that has many applications. (And, I believe, many more applications are waiting to be discovered.)

Rejection Sampling in General

Let’s now discuss rejection sampling in a bit more generality. Say I have a list of n things each of which has a weight w_i\ge 0. Our goal is to choose a random index I with probability proportional to w_i, i.e., \prob \{ I = i\} = w_i / \sum_{j=1}^n w_j. We will call w the target distribution. (Note that we do not require the weights w_i to be normalized to satisfy \sum_{i=1}^n w_i =1.)

Suppose that sampling from the target distribution is challenging, but we can sample from a proposal distribution \rho, i.e., we can efficiently generate random J such that \prob \{J = i\} = \rho_i / \sum_{j=1}^n \rho_j. Further, suppose that the proposal distribution dominates the target distribution in the sense that

    \[w_i \le \rho_i \quad \text{for each } i=1,\ldots,n.\]

Under this general setting, we can sample I from the target distribution using rejection sampling, similar to above:

  1. Propose. Draw a random row index J from the proposal distribution.
  2. Accept/reject. Make a random choice: With probability p_J = w_J/\rho_J, accept and set I\gets J. With the remaining probability 1-p_J, reject and return to step 1.

We recognize the squared row-norm sampling above as an example of this general strategy with w_i = \norm{a_i}^2 and \rho_i = B for all i.

Let us now convince ourselves more carefully that rejection sampling works. On any given execution of the rejection sampling loop, the probability of proposing index i is \rho_i / \sum_{j=1}^n \rho_j, after which the probability of accepting i is w_i / \rho_i. Therefore, the probability of outputting i at any given loop is

    \[\prob \{\text{$i$ accepted this loop}\} = \frac{\rho_i}{\sum_{j=1}^n \rho_j} \cdot \frac{w_i}{\rho_i} = \frac{w_i}{\sum_{j=1}^n \rho_j}.\]

The probability that any index i on that loop is accepted is thus

    \[\prob \{\text{any accepted this loop}\} = \sum_{i=1}^n \prob \{\text{$i$ accepted this loop}\} = \frac{\sum_{i=1}^n w_i}{\sum_{i=1}^n \rho_i}.\]

The rejection sampling loop accepts with fixed positive probability each execution, so it eventually accepts with 100% probability. Thus, the probability of accepting i conditional on some index being accepted is

    \[\prob \{\text{$i$ accepted this loop} \mid \text{any accepted this loop}\} = \frac{\prob \{\text{$i$ accepted this loop}\}}{\prob \{\text{any accepted this loop}\}} = \frac{w_i}{\sum_{j=1}^n w_j}.\]

Therefore, rejection sampling outputs a sample I from the target distribution w as promised.

As this analysis shows, the probability of accepting on any given execution of the rejection sampling loop is \sum_{i=1}^n w_i / \sum_{i=1}^n \rho_i, the ratio of the total mass of the target w_i to the total mass of the proposal \rho_i. Thus, rejection sampling will have a high acceptance rate if w_i \approx \rho_i and a low acceptance rate if w_i \ll \rho_i. The conclusion for practice is that rejection sampling is only computationally efficient if one has access to a good proposal distribution \rho_i, that is both easy to sample from and close to the target w_i\approx \rho_i.

Here, we have presented rejection sampling as a strategy for sampling from a discrete set of items i=1,\ldots,n, but this not all that rejection sampling can do. Indeed, one can also use rejection sampling for sampling a real-valued parameters x \in \real or a multivariate parameter x \in \real^n from a given (unnormalized) probability density function (or, if one likes, an unnormalized probability measure).

Before moving on, let us make one final observation. A very convenient thing about rejection sampling is that we only need the unnormalized probability weights w_i and \rho_i to implement the procedure, even though the total weights \sum_{j=1}^n w_i and \sum_{j=1}^n \rho_i are necessary to define the sampling probabilities \prob \{I = i\} = w_i / \sum_{j=1}^n w_j and \prob \{J = i\} = \rho_i / \sum_{j=1}^n \rho_j. This fact is necessary for many applications of rejection sampling. For instance, in the randomized Kaczmarz use, rejection sampling would be much less useful if we needed the total weight \sum_{i=1}^n \norm{a_i}^2 = \norm{A}_{\rm F}^2, as computing \norm{A}_{\rm F}^2 requires a full pass over the data to compute.

Application: Randomly pivoted Cholesky

Another application of rejection sampling appears is to accelerate the randomly pivoted Cholesky algorithm, the subject of my recent paper. Here, I’ll provide an overview of the main idea with a focus on the role of rejection sampling in the procedure. See the paper for more details. Warning: Even as simplified here, this section presents a significantly more involved application of rejection sampling than we saw previously with randomized Kaczmarz!

Randomly pivoted Cholesky (RPCholesky) is a simple, but powerful algorithm for computing a low-rank approximation to a symmetric positive semidefinite matrix A, and it can be used to accelerate kernel machine learning algorithms.

Conceptually, RPCholesky works as follows. Let A^{(0)} \coloneqq A denote the initial matrix and \hat{A}^{(0)} \coloneqq 0 denote a trivial initial approximation. For j=0,1,2,\ldots,k-1, RPCholesky performs the following steps:

  1. Random sampling. Draw a random index I_{j+1} with probability \prob \{ I_{j+1} = i\} = A^{(j)}_{ii} / \sum_{i=1}^n A^{(j)}_{ii}.
  2. Update approximation. Update \hat{A}^{(j+1)} \gets \hat{A}^{(j)} + a_i^{(j)}(a_i^{(j)})^\top / A_{ii}^{(j)}. Here, a_i^{(j)} denotes the ith column of A^{(j)}.
  3. Update matrix. Update A^{(j+1)} \gets A^{(j)} + a_i^{(j)}(a_i^{(j)})^\top / A_{ii}^{(j)}.

The result of this procedure is a rank-k approximation \hat{A}^{(k)}. With an optimized implementation, RPCholesky requires only O(k^2N) operations and evaluates just (k+1)N entries of the input matrix A.

The standard RPCholesky algorithm is already fast, but there is room for improvement. The standard RPCholesky method processes the matrix A one column a_i at a time, but modern computers are faster at processing blocks of columns. Using the power of rejection sampling, we can develop faster versions of RPCholesky that take advantage of blocked computations. These blocked implementations are important: While we could handle a million-by-million matrix using the standard RPCholesky method, blocked implementations can be up to 40\times faster. In this post, I’ll describe the simplest way of using rejection sampling to implement RPCholesky.

To set the stage, let’s first establish some notation and make a few observations. Let S_j = \{I_1,\ldots,I_j\} denote the first j selected random indices. With a little matrix algebra, one can show that the approximation \hat{A}^{(j)} produced by j steps of RPCholesky obeys the formula1For those interested, observe that \hat{A}^{(j)} is an example of a Nyström approximation. The connection between Nyström approximation and Cholesky decomposition is explained in this previous post of mine.

(1)   \[\hat{A}^{(j)} = A(:,S_j) A(S_j,S_j)^{-1}A(S_j,:). \]

Here, we are using MATLAB notation for indexing the matrix A. The residual matrix A^{(j)} is given by

    \[A^{(j)} = A - \hat{A}^{(j)} = A - A(:,S_j) A(S_j,S_j)^{-1}A(S_j,:).\]

Importantly for us, observe that we can evaluate the ith diagonal entry of A^{(j)} using the formula

(2)   \[A^{(j)}_{ii} = A_{ii} - A(i,S_j) A(S_j,S_j)^{-1} A(S_j,i).\]

Compared to operating on the full input matrix A, evaluating an entry A^{(j)}_{ii} is cheap, just requiring some arithmetic involving matrices and vectors of size j.

Here, we see a situation similar to randomized Kaczmarz. At each step of RPCholesky, we must sample a random index I_{j+1} from a target distribution w_i = A_{ii}^{(j)}, but it is expensive to evaluate all of the w_i‘s. This is a natural setting for rejection sampling. As proposal distribution, we may use the initial diagonal of A, \rho_i = A_{ii}. (One may verify that, as required, w_i = A_{ii}^{(j)} \le A_{ii} = \rho_i for all i.) This leads to a rejection sampling implementation for RPCholesky:

  1. Sample indices. For j=0,1,\ldots,k-1, sample random indices I_{j+1} from the target distribution w_i = A^{(j)}_{ii} using rejection sampling with proposal distribution \rho_i = A_{ii}. Entries A_{ii}^{(j)} are evaluated on an as-needed basis using (2).
  2. Build the approximation. Form the approximation \hat{A}^{(k)} all at once using (1).

By using rejection sampling, we have gone from an algorithm which handles the matrix one column at a time to a new algorithm which processes columns of the matrix A all at once through the formula (1). In the right situations, this new algorithm can be significantly faster than the original RPCholesky method.2In its essence, this rejection sampling algorithm for RPCholesky was first proposed in this paper of mine, which uses rejection sampling to apply RPCholesky to infinite-dimensional positive definite kernel operators. The ability to handle infinite-dimensional sampling problems is another great strength of the rejection sampling approach.

We have now seen two extreme cases: the standard RPCholesky algorithm that processes the columns of A one at a time and a rejection sampling implementation that operates on the columns of A all at once. In practice, the fastest algorithm sits between these extremes, using rejection sampling to sample column indices in moderate-size blocks (say, between 100 and 1000 columns at a time). This “goldilocks” algorithm is the accelerated RPCholesky method that we introduce in our paper. Check it out for details!

Conclusion: Rejection Sampling, an Algorithm Design Tool

We’ve now seen two applications, randomized Kaczmarz and randomly pivoted Cholesky, where rejection sampling can be used to speed up an algorithm. In both cases, we wanted to sample from a distribution over n row or column indices, but it was expensive to perform a census to compute the probability weight of each item individually. Rejection sampling offers a different approach, where we generate samples from a cheap-to-sample proposal distribution and only evaluate the probability weights of the proposed items. In the right situations, this rejection sampling approach can lead to significant computational speedups.

Rejection sampling has been used by statistics-oriented folks for decades, but the power of this technique seems less well-known to researchers in applied math, scientific computation, and related areas. I think there are a lot more exciting ways that we can use rejection sampling to design better, faster randomized algorithms.

Neat Randomized Algorithms: RandDiag for Rapidly Diagonalizing Normal Matrices

Consider two complex-valued square matrices A\in\complex^{n\times n} and B\in\complex^{n\times n}. The first matrix A is Hermitian, being equal A = A^* to its conjugate transpose A^*. The other matrix B is non-Hermitian, B \ne B^*. Let’s see how long it takes to compute their eigenvalue decompositions in MATLAB:

>> A = randn(1e3) + 1i*randn(1e3); A = (A+A')/2;
>> tic; [V_A,D_A] = eig(A); toc % Hermitian matrix
Elapsed time is 0.415145 seconds.
>> B = randn(1e3) + 1i*randn(1e3);
>> tic; [V_B,D_B] = eig(B); toc % non-Hermitian matrix
Elapsed time is 1.668246 seconds.

We see that it takes 4\times longer to compute the eigenvalues of the non-Hermitian matrix B as compared to the Hermitian matrix A. Moreover, the matrix V_A of eigenvectors for a Hermitian matrix A = V_AD_AV_A^{-1} is a unitary matrix, V_A^*V_A = V_AV_A^* = I.

There are another class of matrices with nice eigenvalue decompositions, normal matrices. A square, complex-valued matrix C is normal if C^*C = CC^*. The matrix V_C of eigenvectors for a normal matrix C = V_C D_C V_C^{-1} is also unitary, V_C^*V_C = V_CV_C^* = I. An important class of normal matrices are unitary matrices themselves. A unitary matrix U is always normal since it satisfies U^*U = UU^* = I.

Let’s see how long it takes MATLAB to compute the eigenvalue decomposition of a unitary (and thus normal) matrix:

>> U = V_A;                     % unitary, and thus normal, matrix
>> tic; [V_U,D_U] = eig(U); toc % normal matrix
Elapsed time is 2.201017 seconds.

Even longer than it took to compute an eigenvalue decomposition of the non-normal matrix B! Can we make the normal eigenvalue decomposition closer to the speed of the Hermitian eigenvalue decomposition?

Here is the start of an idea. Every square matrix C has a Cartesian decomposition:

    \[C = H + iS, \quad H = \frac{C+C^*}{2}, \quad S = \frac{C-C^*}{2i}.\]

We have written C as a combination of its Hermitian part H and i times its skew-Hermitian part S. Both H and S are Hermitian matrices. The Cartesian decomposition of a square matrix is analogous to the decomposition of a complex number into its real and imaginary parts.

For a normal matrix C, the Hermitian and skew-Hermitian parts commute, HS = SH. We know from matrix theory that commuting Hermitian matrices are simultaneously diagonalizable, i.e., there exists Q such that H = QD_HQ^* and S = QD_SQ^* for diagonal matrices D_H and D_S. Thus, given access to such Q, C has eigenvalue decomposition

    \[C = Q(D_H+iD_S)Q^*.\]

Here’s a first attempt to turn this insight into an algorithm. First, compute the Hermitian part H of C, diagonalize H = QD_HQ^*, and then see if Q diagonalizes C. Let’s test this out on a 2\times 2 example:

>> C = orth(randn(2) + 1i*randn(2)); % unitary matrix
>> H = (C+C')/2;                     % Hermitian part
>> [Q,~] = eig(H);
>> Q'*C*Q                            % check to see if diagonal
ans =
  -0.9933 + 0.1152i  -0.0000 + 0.0000i
   0.0000 + 0.0000i  -0.3175 - 0.9483i

Yay! We’ve succeeded at diagonalizing the matrix C using only a Hermitian eigenvalue decomposition. But we should be careful about declaring victory too early. Here’s a bad example:

>> C = [1 1i;1i 1]; % normal matrix
>> H = (C+C')/2;
>> [Q,~] = eig(H);
>> Q'*C*Q           % oh no! not diagonal
ans =
   1.0000 + 0.0000i   0.0000 + 1.0000i
   0.0000 + 1.0000i   1.0000 + 0.0000i

What’s going on here? The issue is that the Hermitian part H = I for this matrix has a repeated eigenvalue. Thus, H has multiple different valid matrices of eigenvectors. (In this specific case, every unitary matrix Q diagonalizes H.) By looking at H alone, we don’t know which Q matrix to pick which also diagonalizes S.

He and Kressner developed a beautifully simple randomized algorithm called RandDiag to circumvent this failure mode. The idea is straightforward:

  1. Form a random linear combination M = \gamma_1 H + \gamma_2 S of the Hermitian and skew-Hermitian parts of A, with standard normal random coefficients \gamma_1 and \gamma_2.
  2. Compute Q that diagonalizes M.

That’s it!

To get a sense of why He and Kressner’s algorithm works, suppose that H has some repeated eigenvalues and S has all distinct eigenvalues. Given this setup, it seems likely that a random linear combination of S and H will also have all distinct eigenvalues. (It would take a very special circumstances for a random linear combination to yield two eigenvalues that are exactly the same!) Indeed, this intuition is a fact: With 100% probability, Q diagonalizing a Gaussian random linear combination of simultaneously diagonalizable matrices H and S also diagonalizes H and S individually.

MATLAB code for RandDiag is as follows:

function Q = rand_diag(C)
   H = (C+C')/2; S = (C-C')/2i;
   M = randn*H + randn*S;
   [Q,~] = eig(M);
end

When applied to our hard 2\times 2 example from before, RandDiag succeeds at giving a matrix that diagonalizes C:

>> Q = rand_diag(C);
>> Q'*C*Q
ans =
   1.0000 - 1.0000i  -0.0000 + 0.0000i
  -0.0000 - 0.0000i   1.0000 + 1.0000i

For computing the matrix of eigenvectors for a 1000\times 1000 unitary matrix, RandDiag takes 0.4 seconds, just as fast as the Hermitian eigendecomposition did.

>> tic; V_U = rand_diag(U); toc
Elapsed time is 0.437309 seconds.

He and Kressner’s algorithm is delightful. Ultimately, it uses randomness in only a small way. For most coefficients a_1,a_2 \in \real, a matrix Q diagonalizing a_1 H + a_2 S will also diagonalize A = H+iS. But, for any specific choice of a_1,a_2, there is a possibility of failure. To avoid this possibility, we can just pick a_1 and a_2 at random. It’s really as simple as that.

References: RandDiag was proposed in A simple, randomized algorithm for diagonalizing normal matrices by He and Kressner (2024), building on their earlier work in Randomized Joint Diagonalization of Symmetric Matrices (2022) which considers the general case of using random linear combinations to (approximately) simultaneous diagonalize (nearly) commuting matrices. RandDiag is an example of a linear algebraic algorithm that uses randomness to put the input into “general position”; see Randomized matrix computations: Themes and variations by Kireeva and Tropp (2024) for a discussion of this, and other, ways of using randomness to design matrix algorithms.

Neat Randomized Algorithms: Randomized Cholesky QR

As a research area, randomized numerical linear algebra (RNLA) is as hot as ever. To celebrate the exciting work in this space, I’m starting a new series on my blog where I celebrate cool recent algorithms in the area. At some future point, I might talk about my own work in this series, but for now I’m hoping to use this series to highlight some of the awesome work being done by my colleagues.


Given a tall matrix A \in \real^{m\times n} with m\ge n, its (economy-size) QR factorization is a decomposition of the form A = QR, where Q \in \real^{m\times n} is a matrix with orthonormal columns and R \in \real^{n\times n} is upper triangular. QR factorizations are used to solve least-squares problems and as a computational procedure to orthonormalize the columns of a matrix.

Here’s an example in MATLAB, where we use QR factorization to orthonormalize the columns of a 10^6\times 10^2 test matrix. It takes about 2.5 seconds to run.

>> A = randn(1e6, 1e2) * randn(1e2) * randn(1e2); % test matrix
>> tic; [Q,R] = qr(A,"econ"); toc
Elapsed time is 2.647317 seconds.

The classical algorithm for computing a QR factorization uses Householder reflectors and is exceptionally numerically stable. Since Q has orthonormal columns, Q^\top Q = I is the identity matrix. Indeed, this relation holds up to a tiny error for the Q computed by Householder QR:

>> norm(Q'*Q - eye(1e2)) % || Q^T Q - I ||
ans =
   7.0396e-14

The relative error \|A - QR\|/\|A\| is also small:

>> norm(A - Q*R) / norm(A)
ans =
   4.8981e-14

Here is an alternate procedure for computing a QR factorization, known as Cholesky QR:

function [Q,R] = cholesky_qr(A)
   R = chol(A'*A);
   Q = A / R;       % Q = A * R^{-1}
end

This algorithm works by forming A^\top A, computing its (upper triangular) Cholesky decomposition A^\top A = R^\top R, and setting Q = AR^{-1}. Cholesky QR is very fast, about 5\times faster than Householder QR for this example:

>> tic; [Q,R] = cholesky_qr(A); toc
Elapsed time is 0.536694 seconds.

Unfortunately, Cholesky QR is much less accurate and numerically stable than Householder QR. Here, for instance, is the value of \|Q^\top Q - I\|, about ten million times larger than for Householder QR!:

>> norm(Q'*Q - eye(1e2))
ans =
   7.5929e-07

What’s going on? As we’ve discussed before on this blog, forming A^\top A is typically problematic in linear algebraic computations. The “badness” of a matrix A is measured by its condition number, defined to be the ratio of its largest and smallest singular values \kappa(A) = \sigma_{\rm max}(A)/\sigma_{\rm min}(A). The condition number of A^\top A is the square of the condition number of A, \kappa(A^\top A) = \kappa(A)^2, which is at the root of Cholesky QR’s loss of accuracy. Thus, Cholesky QR is only appropriate for matrices that are well-conditioned, having a small condition number \kappa(A) \approx 1, say \kappa(A) \le 10.

The idea of randomized Cholesky QR is to use randomness to precondition A, producing a matrix R_1 that B = AR_1^{-1} is well-conditioned. Then, since B is well-conditioned, we can apply ordinary Cholesky QR to it without issue. Here are the steps:

  1. Draw a sketching matrix S of size 2n\times m; see these posts of mine for an introduction to sketching.
  2. Form the sketch SA. This step compresses the very tall matrix m\times n to the much shorter matrix SA of size 2n\times n.
  3. Compute a QR factorization SA = Q_1R_1 using Householder QR. Since the matrix SA is small, this factorization will be quick to compute.
  4. Form the preconditioned matrix B = AR_1^{-1}.
  5. Apply Cholesky QR to B to compute B = QR_2.
  6. Set R = R_2R_1. Observe that A = BR_1 = QR_2R_1 = QR, as desired.

MATLAB code for randomized Cholesky QR is provided below:1Code for the sparsesign subroutine can be found here.

function [Q,R] = rand_cholesky_qr(A)
   S = sparsesign(2*size(A,2),size(A,1),8); % sparse sign embedding
   R1 = qr(S*A,"econ"); % sketch and (Householder) QR factorize
   B = A / R1; % B = A * R_1^{-1}
   [Q,R2] = cholesky_qr(B);
   R = R2*R1;
end

Randomized Cholesky QR is still faster than ordinary Householder QR, about 3\times faster in our experiment:

>> tic; [Q,R] = rand_cholesky_qr(A); toc
Elapsed time is 0.920787 seconds.

Randomized Cholesky QR greatly improves on ordinary Cholesky QR in terms of accuracy and numerical stability. In fact, the size of \|Q^\top Q - I\| is even smaller than for Householder QR!

>> norm(Q'*Q - eye(1e2))
ans =
   1.0926e-14

The relative error \|A - QR\|/\|A\| is small, too! Even smaller than for Householder QR in fact:

>> norm(A - Q*R) / norm(A)
ans =
   4.0007e-16

Like many great ideas, randomized Cholesky QR was developed independently by a number of research groups. A version of this algorithm was first introduced in 2021 by Fan, Guo, and Lin. Similar algorithms were investigated in 2022 and 2023 by Balabanov, Higgins et al., and Melnichenko et al. Check out Melnichenko et al.‘s paper in particular, which shows very impressive results for using randomized Cholesky QR to compute column pivoted QR factorizations.

References: Primary references are A Novel Randomized XR-Based Preconditioned CholeskyQR Algorithm by Fan, Guo, and Lin (2021); Randomized Cholesky QR factorizations by Balabanov (2022); Analysis of Randomized Householder-Cholesky QR Factorization with Multisketching by Higgins et al. (2023); CholeskyQR with Randomization and Pivoting for Tall Matrices (CQRRPT) by Melnichenko et al. (2023). The idea of using sketching to precondition tall matrices originates in the paper A fast randomized algorithm for overdetermined linear least-squares regression by Rokhlin and Tygert (2008).

Note to Self: Gaussian Hypercontractivity

The purpose of this note is to describe the Gaussian hypercontractivity inequality. As an application, we’ll obtain a weaker version of the Hanson–Wright inequality.

The Noise Operator

We begin our discussion with the following question:

Let f : \real^n \to \real be a function. What happens to f, on average, if we perturb its inputs by a small amount of Gaussian noise?

Let’s be more specific about our noise model. Let x \in \real^n be an input to the function f and fix a parameter 0 \le \varrho \le 1 (think of \varrho as close to 1). We’ll define the noise corruption of x to be

(1)   \[\tilde{x}_\varrho = \varrho \cdot x + \sqrt{1-\varrho^2} \cdot g, \quad \text{where } g\sim \operatorname{Normal}(0,I). \]

Here, \operatorname{Normal}(0,I) is the standard multivariate Gaussian distribution. In our definition of \tilde{x}_\varrho, we both add Gaussian noise \sqrt{1-\varrho^2} \cdot g and shrink the vector x by a factor \varrho. In particular, we highlight two extreme cases:

  • No noise. If \varrho = 1, then there is no noise and \tilde{x}_\varrho = x.
  • All noise. If \varrho = 0, then there is all noise and \tilde{x}_\varrho = g. The influence of the original vector x has been washed away completely.

The noise corruption (1) immediately gives rise to the noise operator1The noise operator is often called the Hermite operator. The noise operator is related to the Ornstein–Uhlenbeck semigroup operator P_t by a change of variables, P_t = U_{\e^{-t}}. T_\varrho. Let f : \real^n \to \real be a function. The noise operator T_\varrho is defined to be:

(2)   \[(T_\varrho f)(x) = \expect[f(\tilde{x}_\varrho)] = \expect_{g\sim \operatorname{Normal}(0,I)}[f( \varrho \cdot x + \sqrt{1-\varrho^2}\cdot g)]. \]

The noise operator computes the average value of f when evaluated at the noisy input \tilde{x}_\varrho. Observe that the noise operator maps a function f : \real^n \to \real to another function T_\varrho f : \real^n \to \real. Going forward, we will write T_\varrho f(x) to denote (T_\varrho f)(x).

To understand how the noise operator acts on a function f, we can write the expectation in the definition (2) as an integral:

    \[T_\varrho f(x) = \int_{\real^d} f(\varrho x + y) \frac{1}{(2\pi (1-\varrho^2))^{d/2}}\e^{-\frac{|y|^2}{2(1-\varrho^2)}} \, \mathrm{d} y.\]

Here, |y| denotes the (Euclidean) length of y\in\real^d. We see that T_\varrho f is the convolution of f(\varrho x) with a Gaussian density. Thus, T_\varrho acts to smooth the function f.

See below for an illustration. The red solid curve is a function f, and the blue dashed curve is T_{0.95}f.

As we decrease \varrho from 1 to 0, the function T_\varrho f is smoothed more and more. When we finally reach \varrho = 0, T_\varrho f has been smoothed all the way into a constant.

Random Inputs

The noise operator converts a function f to another function T_\varrho f. We can evaluate these two functions at a Gaussian random vector x\sim \operatorname{Normal}(0,I), resulting in two random variables f(x) and T_\varrho f(x).

We can think of T_\varrho f(x) as a modification of the random variable f(x) where “a 1-\varrho^2 fraction of the variance of x has been averaged out”. We again highlight the two extreme cases:

  • No noise. If \varrho = 1, T_\varrho f(x) = f(x). None of the variance of x has been averaged out.
  • All noise. If \varrho=0,T_\varrho f(x) = \expect_{g\sim\operatorname{Normal}(0,I)}[f(g)] is a constant random variable. All of the variance of x has been averaged out.

Just as decreasing \varrho smoothes the function T_\varrho f until it reaches a constant function at \varrho = 0, decreasing \varrho makes the random variable T_\varrho f(x) more and more “well-behaved” until it becomes a constant random variable at \varrho = 0. This “well-behavingness” property of the noise operator is made precise by the Gaussian hypercontractivity theorem.

Moments and Tails

In order to describe the “well-behavingness” properties of the noise operator, we must answer the question:

How can we measure how well-behaved a random variable is?

There are many answers to this question. For this post, we will quantify the well-behavedness of a random variable by using the L_p norm.2Using norms is a common way of measuring the niceness of a function or random variable in applied math. For instance, we can use Sobolev norms or reproducing kernel Hilbert space norms to measure the smoothness of a function in approximation theory, as I’ve discussed before on this blog.

The L_p norm of a (\real-valued) random variable y is defined to be

(3)   \[\norm{y}_p \coloneqq \left( \expect[|y|^p] \right)^{1/p}.\]

The pth power of the L_p norm \norm{y}_p^p is sometimes known as the pth absolute moment of y.

The L_p norms of random variables control the tails of a random variable—that is, the probability that a random variable is large in magnitude. A random variables with small tails is typically thought of as a “nice” or “well-behaved” random variable. Random quantities with small tails are usually desirable in applications, as they are more predictable—unlikely to take large values.

The connection between tails and L_p norms can be derived as follows. First, write the tail probability \prob \{|y| \ge t\} for t > 0 using pth powers:

    \[\prob \{|y| \ge t\} = \prob\{ |y|^p \ge t^p \}.\]

Then, we apply Markov’s inequality, obtaining

(4)   \[\prob \{|y| \ge t\} = \prob \{ |y|^p \ge t^p \} \le \frac{\expect [|y|^p]}{t^p} = \frac{\norm{y}_p^p}{t^p}.\]

We conclude that a random variable with finite L_p norm (i.e., \norm{y}_p < +\infty) has tails that decay at at a rate 1/t^p or faster.

Gaussian Contractivity

Before we introduce the Gaussian hypercontractivity theorem, let’s establish a weaker property of the noise operator, contractivity.

Proposition 1 (Gaussian contractivity). Choose a noise level 0 < \varrho \le 1 and a power p\ge 1, and let x\sim \operatorname{Normal}(0,I) be a Gaussian random vector. Then T_\varrho contracts the L_p norm of f(x):

    \[\norm{T_\varrho f(x)}_p \le \norm{f(x)}_p.\]

This result shows that the noise operator makes the random variable T_\varrho f(x) no less nice than f(x) was.

Gaussian contractivity is easy to prove. Begin using the definition of the noise operator (2) and L_p norm (3):

    \[\norm{T_\varrho f(x)}_p^p = \expect_{x\sim \operatorname{Normal}(0,I)} \left[ \left|\expect_{g\sim \operatorname{Normal}(0,I)}[f(\varrho x + \sqrt{1-\varrho^2}\cdot g)]\right|^p\right]\]

Now, we can apply Jensen’s inequality to the convex function t\mapsto t^p, obtaining

    \[\norm{T_\varrho f(x)}_p^p \le \expect_{x,g\sim \operatorname{Normal}(0,I)} \left[ \left|f(\varrho x + \sqrt{1-\varrho^2}\cdot g)\right|^p\right].\]

Finally, realize that for the independent normal random vectorsx,g\sim \operatorname{Normal}(0,I), we have

    \[\varrho x + \sqrt{1-\varrho^2}\cdot g \sim \operatorname{Normal}(0,I).\]

Thus, \varrho x + \sqrt{1-\varrho^2}\cdot g has the same distribution as x. Thus, using x in place of \varrho x + \sqrt{1-\varrho^2}\cdot g, we obtain

    \[\norm{T_\varrho f(x)}_p^p \le \expect_{x\sim \operatorname{Normal}(0,I)} \left[ \left|f(x)\right|^p\right] = \norm{f(x)}_p^p.\]

Gaussian contractivity (Proposition 1) is proven.

Gaussian Hypercontractivity

The Gaussian contractivity theorem shows that T_\varrho f(x) is no less well-behaved than f(x) is. In fact, T_\varrho f(x) is more well-behaved than f is. This is the content of the Gaussian hypercontractivity theorem:

Theorem 2 (Gaussian hypercontractivity): Choose a noise level 0 < \varrho \le 1 and a power p\ge 1, and let x\sim \operatorname{Normal}(0,I) be a Gaussian random vector. Then

    \[\norm{T_\varrho f(x)}_{1+(p-1)/\varrho^2} \le \norm{f(x)}_p.\]

In particular, for p=2,

    \[\norm{T_\varrho f(x)}_{1+\varrho^{-2}} \le \norm{f(x)}_2.\]

We have highlighted the p=2 case because it is the most useful in practice.

This result shows that as we take \varrho smaller, the random variable T_\varrho f(x) becomes more and more well-behaved, with tails decreasing at a rate

    \[\prob \{ |T_\varrho f(x)| \ge t \} \le \frac{\norm{T_\varrho f(x)}_{1+(p-1)/\varrho^2}}{t^{1 + (p-1)/\varrho^2}} \le \frac{\norm{f(x)}_p}{t^{1 + (p-1)/\varrho^2}}.\]

The rate of tail decrease becomes faster and faster as \varrho becomes closer to zero.

We will prove the Gaussian hypercontractivity at the bottom of this post. For now, we will focus on applying this result.

Multilinear Polynomials

A multilinear polynomial f(x) = f(x_1,\ldots,x_d) is a multivariate polynomial in the variables x_1,\ldots,x_d in which none of the variables x_1,\ldots,x_d is raised to a power higher than one. So,

(5)   \[1+x_1x_2\]

is multilinear, but

    \[1+x_1+x_1x_2^\]

is not multilinear (since x_2 is squared).

For multilinear polynomials, we have the following very powerful corollary of Gaussian hypercontractivity:

Corollary 3 (Absolute moments of a multilinear polynomial of Gaussians). Let f be a multilinear polynomial of degree k. (That is, at most k variables x_{i_1}\cdots x_{i_k} occur in any monomial of f.) Then, for a Gaussian random vector x\sim \operatorname{Normal}(0,I) and for all q \ge 2,

    \[\norm{f(x)}_q \le (q-1)^{k/2} \norm{f(x)}_2.\]

Let’s prove this corollary. The first observation is that the noise operator has a particularly convenient form when applied to a multilinear polynomial. Let’s test it out on our example (5) from above. For

    \[f(x) = 1+x_1x_2,\]

we have

    \begin{align*}T_\varrho f(x) &= \expect_{g_1,g_2 \sim \operatorname{Normal}(0,1)} \left[1+ (\varrho x_1 + \sqrt{1-\varrho^2}\cdot g_1)(\varrho x_2 + \sqrt{1-\varrho^2}\cdot g_2)\right].\\&= 1 + \expect[\varrho x_1 + \sqrt{1-\varrho^2}\cdot g_1]\expect[\varrho x_2 + \sqrt{1-\varrho^2}\cdot g_2]\\&= 1+ (\varrho x_1)(\varrho x_2) \\&= f(\varrho x).\end{align*}

We see that the expectation applies to each variable separately, resulting in each x_i replaced by \varrho x_i. This trend holds in general:

Proposition 4 (noise operator on multilinear polynomials). For any multilinear polynomial f, T_\varrho f(x) = f(\varrho x).

We can use Proposition 4 to obtain bounds on the L_p norms of multilinear polynomials of a Gaussian random variable. Indeed, observe that

    \[f(x) = f(\varrho \cdot x/\varrho) = T_\varrho f(x/\varrho).\]

Thus, by Gaussian hypercontractivity, we have

    \[\norm{f(x)}_{1+\varrho^{-2}}=\norm{T_\varrho f(x/\varrho)}_{1+\varrho^{-2}} \le \norm{f(x/\varrho)}_2.\]

The final step of our argument will be to compute \norm{f(x/\varrho)}_2. Write f as

    \[f(x) = \sum_{i_1,\ldots,i_s} a_{i_1,\ldots,i_s} x_{i_1} \cdots x_{i_s}.\]

Since f is multilinear, i_j\ne i_\ell for j\ne \ell. Since f is degree-k, s\le k. The multilinear monomials x_{i_1}\cdots x_{i_s} are orthonormal with respect to the L_2 inner product:

    \[\expect[(x_{i_1}\cdots x_{i_s}) \cdot (x_{i_1'}\cdots x_{i_s'})] = \begin{cases} 0 &\text{if } \{i_1,\ldots,i_s\} \ne \{i_1',\ldots,i_{s'}\}, \\1, & \text{otherwise}.\end{cases}\]

(See if you can see why!) Thus, by the Pythagorean theorem, we have

    \[\norm{f(x)}_2^2 = \sum_{i_1,\ldots,i_s} a_{i_1,\ldots,i_s}^2.\]

Similarly, the coefficients of f(x/\varrho) are a_{i_1,\ldots,i_s} / \varrho. Thus,

    \[\norm{f(x/\varrho)}_2^2 = \sum_{i_1,\ldots,i_s} \varrho^{-2s} a_{i_1,\ldots,i_s}^2 \le \varrho^{-2k} \sum_{i_1,\ldots,i_s} a_{i_1,\ldots,i_s}^2 = \varrho^{-2k}\norm{f(x)}_2^2.\]

Thus, putting all of the ingredients together, we have

    \[\norm{f(x)}_{1+\varrho^{-2}}=\norm{T_\varrho f(x/\varrho)}_p \le \norm{f(x/\varrho)}_2 \le \varrho^{-k} \norm{f(x)}_2.\]

Setting q = 1+\varrho^{-2} (equivalently \varrho = 1/\sqrt{q-1}), Corollary 3 follows.

Hanson–Wright Inequality

To see the power of the machinery we have developed, let’s prove a version of the Hanson–Wright inequality.

Theorem 5 (suboptimal Hanson–Wright). Let A be a symmetric matrix with zero on its diagonal and x\sim \operatorname{Normal}(0,I) be a Gaussian random vector. Then

    \[\prob \{|x^\top A x| \ge t \} \le \exp\left(- \frac{t}{\sqrt{2}\mathrm{e}\norm{A}_{\rm F}} \right) \quad \text{for } t\ge \sqrt{2}\mathrm{e}\norm{A}_{\rm F}.\]

Hanson–Wright has all sorts of applications in computational mathematics and data science. One direct application is to obtain probabilistic error bounds for the error incurred by a stochastic trace estimation formulas.

This version of Hanson–Wright is not perfect. In particular, it does not capture the Bernstein-type tail behavior of the classical Hanson–Wright inequality

    \[\prob\{|x^\top Ax| \ge t\} \le 2\exp \left( -\frac{t^2}{4\norm{A}_{\rm F}^2+4\norm{A}t} \right).\]

But our suboptimal Hanson–Wright inequality is still pretty good, and it requires essentially no work to prove using the hypercontractivity machinery. The hypercontractivity technique also generalizes to settings where some of the proofs of Hanson–Wright fail, such as multilinear polynomials of degree higher than two.

Let’s prove our suboptimal Hanson–Wright inequality. Set f(x) = x^\top Ax. Since A has zero on its diagonal, f is a multilinear polynomial of degree two in the entries of x. The random variable f(x) is mean-zero, and a short calculation shows its L_2 norm is

    \[\norm{f(x)}_2 = \sqrt{\Var(f(x))} = \sqrt{2} \norm{A}_{\rm F}.\]

Thus, by Corollary 3,

(6)   \[\norm{f(x)}_q \le (q-1) \norm{f(x)}_2 \le \sqrt{2} q \norm{A}_{\rm F} \quad \text{for every } q\ge 2. \]

In fact, since the L_q norms are monotone, (6) holds for 1\le q\le 2 as well. Therefore, the standard tail bound for L_q norms (4) gives

(7)   \[\prob \{|x^\top A x| \ge t \} \le \frac{\norm{f(x)}_q^q}{t^q} \le \left( \frac{\sqrt{2}q\norm{A}_{\rm F}}{t} \right)^q\quad \text{for }q\ge 1.\]

Now, we must optimize the value of q to obtain the sharpest possible bound. To make this optimization more convenient, introduce a parameter

    \[\alpha \coloneqq \frac{\sqrt{2}q\norm{A}_{\rm F}}{t}.\]

In terms of the \alpha parameter, the bound (7) reads

    \[\prob \{|x^\top A x| \ge t \} \le \exp\left(- \frac{t}{\sqrt{2}\norm{A}_{\rm F}} \alpha \ln \frac{1}{\alpha} \right) \quad \text{for } t\ge \frac{\sqrt{2}\norm{A}_{\rm F}}{\alpha}.\]

The tail bound is minimized by taking \alpha = 1/\mathrm{e}, yielding the claimed result

    \[\prob \{|x^\top A x| \ge t \} \le \exp\left(- \frac{t}{\sqrt{2}\mathrm{e}\norm{A}_{\rm F}} \right) \quad \text{for } t\ge \sqrt{2}\mathrm{e}\norm{A}_{\rm F}.\]

Proof of Gaussian Hypercontractivity

Let’s prove the Gaussian hypercontractivity theorem. For simplicity, we will stick with the d = 1 case, but the higher-dimensional generalizations follow along similar lines. The key ingredient will be the Gaussian Jensen inequality, which made a prominent appearance in a previous blog post of mine. Here, we will only need the following version:

Theorem 6 (Gaussian Jensen). Let b : \real^2 \to \real be a twice differentiable function and let (x,\tilde{x}) \sim \operatorname{Normal}(0,\Sigma) be jointly Gaussian random variables with covariance matrix \Sigma. Then

(8)   \[b(\expect[h_1(x)], \expect[h_2(\tilde{x})]) \ge \expect [b(h_1(x),h_2(\tilde{x}))]\]

holds for all test functions h_1,h_2 : \real \to \real if, and only if,

(9)   \[\Sigma \circ \nabla^2 b \quad\text{is negative semidefinite on all of $\real^2$}.\]

Here, \circ denotes the entrywise product of matrices and \nabla^2 b : \real^2\to \real^{2\times 2} is the Hessian matrix of the function b.

To me, this proof of Gaussian hypercontractivity using Gaussian Jensen (adapted from Paata Ivanishvili‘s excellent post) is amazing. First, we reformulate the Gaussian hypercontractivity property a couple of times using some functional analysis tricks. Then we do a short calculation, invoke Gaussian Jensen, and the theorem is proved, almost as if by magic.

Part 1: Tricks

Let’s begin with “tricks” part of the argument.

Trick 1. To prove Gaussian hypercontractivity holds for all functions f, it is sufficient to prove for all nonnegative functions f\ge 0.

Indeed, suppose Gaussian hypercontractivity holds for all nonnegative functions f. Then, for any function f, apply Jensen’s inequality to conclude

    \begin{align*} T_\varrho |f|(x) &= \expect_{g\sim \operatorname{Normal}(0,1)} \left| f(\varrho x+\sqrt{1-\varrho^2}\cdot g)\right| \\&\ge \left| \expect_{g\sim \operatorname{Normal}(0,1)} f(\varrho x+\sqrt{1-\varrho^2}\cdot g)\right| \\&= |T_\varrho f(x)|.\end{align*}

Thus, assuming hypercontractivity holds for the nonnegative function |f|, we have

    \[\norm{T_\varrho f(x)}_{1+(p-1)/\varrho^2} \le \norm{T_\varrho |f|(x)}_{1+(p-1)/\varrho^2} \le \norm{|f|(x)}_p = \norm{f}_p.\]

Thus, the conclusion of the hypercontractivity theorem holds for f as well, and the Trick 1 is proven.

Trick 2. To prove Gaussian hypercontractivity for all f\ge 0, it is sufficient to prove the following “bilinearized” Gaussian hypercontractivity result:

    \[\expect[g(x) \cdot T_\varrho f(x)]\le \norm{g(x)}_{q'} \norm{f(x)}_p\]

holds for all g\ge 0 with \norm{g(x)}_{q'} < +\infty. Here, q'=q/(q-1) is the Hölder conjugate to q = 1+(p-1)/\varrho^2.

Indeed, this follows3This argument may be more clear to parse if we view f and g as functions on \real equipped with the standard Gaussian measure \gamma. This result is just duality for the L_q(\gamma) norm. from the dual characterization of the norm of T_\varrho f(x):

    \[\norm{T_\varrho f(x)}_q = \sup_{\substack{\norm{g(x)} < +\infty \\ g\ge 0}} \frac{\expect[g(x) \cdot T_\varrho f(x)]}{\norm{g(x)}_{q'}}.\]

Trick 2 is proven.

Trick 3. Let x,\tilde{x} be a pair of standard Gaussian random variables with correlation \rho. Then the bilinearized Gaussian hypercontractivity statement is equivalent to

    \[\expect[g(x) f(\tilde{x})]\le (\expect[(g(x)^{q'})])^{1/q'} (\expect[(f(\tilde{x})^{p})])^{1/p}.\]

Indeed, define \tilde{x} = \varrho x + \sqrt{1-\varrho^2} \cdot g for the random variable in the definition of the noise operator T_\varrho. The random variable \tilde{x} is standard Gaussian and has correlation \varrho with f, concluding the proof of Trick 3.

Finally, we apply a change of variables as our last trick:

Trick 4. Make the change of variables u \coloneqq f^p and v \coloneqq g^{q'}, yielding the final equivalent version of Gaussian hypercontractivity:

    \[\expect[v(x)^{1/q'} u(\tilde{x})^{1/p}]\le (\expect[v(x)])^{1/q'} (\expect[u(\tilde{x}))])^{1/p}\]

for all functions u and v (in the appropriate spaces).

Part 2: Calculation

We recognize this fourth equivalent version of Gaussian hypercontractivity as the conclusion (8) to Gaussian Jensen with

    \[b(u,v) = u^{1/p}v^{1/q'}\]

. Thus, to prove Gaussian hypercontractivity, we just need to check the hypothesis (9) of the Gaussian Jensen inequality (Theorem 6).

We now enter the calculation part of the proof. First, we compute the Hessian of b:

    \[\nabla^2 b(u,v) = u^{1/p}v^{1/q'}\cdot\begin{bmatrix} - \frac{1}{pp'} u^{-2} & \frac{1}{pq'} u^{-1}v^{-1} \\ \frac{1}{pq'} u^{-1}v^{-1} & - \frac{1}{qq'} v^{-2}\end{bmatrix}.\]

We have written p' for the Hölder conjugate to p. By Gaussian Jensen, to prove Gaussian hypercontractivity, it suffices to show that

    \[\nabla^2 b(u,v)\circ \twobytwo{1}{\varrho}{\varrho}{1}= u^{1/p}v^{1/q'}\cdot\begin{bmatrix} - \frac{1}{pp'} u^{-2} & \frac{\varrho}{pq'} u^{-1}v^{-1} \\ \frac{\varrho}{pq'} u^{-1}v^{-1} & - \frac{1}{qq'} v^{-2}\end{bmatrix}\]

is negative semidefinite for all u,v\ge 0. There are a few ways we can make our lives easier. Write this matrix as

    \[\nabla^2 b(u,v)\circ \twobytwo{1}{\varrho}{\varrho}{1}= u^{1/p}v^{1/q'}\cdot B^\top\begin{bmatrix} - \frac{p}{p'} & \varrho \\ \varrho & - \frac{q'}{q} \end{bmatrix}B \quad \text{for } B = \operatorname{diag}(p^{-1}u^{-1},(q')^{-1}v^{-1}).\]

Scaling A\mapsto \alpha \cdot A by nonnegative \alpha and conjugation A\mapsto B^\top A B both preserve negative semidefiniteness, so it is sufficient to prove

    \[H = \begin{bmatrix} - \frac{p}{p'} & \varrho \\ \varrho & - \frac{q'}{q} \end{bmatrix} \quad \text{is negative semidefinite}.\]

Since the diagonal entries of H are negative, at least one of H‘s eigenvalues is negative.4Indeed, by the Rayleigh–Ritz variational principle, the smallest eigenvalue of a symmetric matrix H is \lambda_{\rm min}(H) = \min_{\norm{x}=1} x^\top Hx. Taking x = e_i for i=1,2,\ldots to be each of the standard basis vectors, shows that the smallest eigenvalue of A is smaller than the smallest diagonal entry of H. Therefore, to prove H is negative semidefinite, we can prove that its determinant (= product of its eigenvalues) is nonnegative. We compute

    \[\det H = \frac{pq'}{p'q} - \varrho^2 .\]

Now, just plug in the values for p'=p/(p-1), q=1+(p-1)/\varrho^2, q'=q/(q-1):

    \[\det H = \frac{pq'}{p'q} - \varrho^2 = \frac{p-1}{q-1} - \varrho^2 = \frac{p-1}{(p-1)/\varrho^2} - \varrho^2 = 0.\]

Thus, \det H \ge 0. We conclude H is negative semidefinite, proving the Gaussian hypercontractivity theorem.

Don’t Use Gaussians in Stochastic Trace Estimation

Suppose we are interested in estimating the trace \tr(A) = \sum_{i=1}^n A_{ii} of an n\times n matrix A that can be only accessed through matrix–vector products Ax_1,\ldots,Ax_m. The classical method for this purpose is the GirardHutchinson estimator

    \[\hat{\tr} = \frac{1}{m} \left( x_1^\top Ax_1 + \cdots + x_m^\top Ax_m \right),\]

where the vectors x_1,\ldots,x_m are independent, identically distributed (iid) random vectors satisfying the isotropy condition

    \[\expect[x_ix_i^\top] = I.\]

Examples of vectors satisfying this condition include

Stochastic trace estimation has a number of applications: log-determinant computations in machine learningpartition function calculations in statistical physicsgeneralized cross validation for smoothing splines, and triangle counting in large networks. Several improvements to the basic Girard–Hutchinson estimator have been developed recently. I am partial to XTrace, an improved trace estimator that I developed with my collaborators.

This post is addressed at the question:

Which distribution should be used for the test vectors x_i for stochastic trace estimation?

Since the Girard–Hutchinson estimator is unbiased \expect[\hat{\tr}] = \tr(A), the variance of \hat{\tr} is equal to the mean-square error. Thus, the lowest variance trace estimate is the most accurate. In my previous post on trace estimation, I discussed formulas for the variance \Var(\hat{\tr}) of the Girard–Hutchinson estimator with different choices of test vectors. In that post, I stated the formulas for different choices of test vectors (Gaussian, random signs, sphere) and showed how those formulas could be proven.

In this post, I will take the opportunity to editorialize on which distribution to pick. The thesis of this post is as follows:

The sphere distribution is essentially always preferable to the Gaussian distribution for trace estimation.

To explain why, let’s focus on the case when A is real and symmetric.1The same principles hold in the general case, but the variance formulas are more delicate to state. See my previous post for the formulas. Let \lambda_1,\ldots,\lambda_n be the eigenvalues of A and define the eigenvalue mean

    \[\overline{\lambda} = \frac{\lambda_1 + \cdots + \lambda_n}{n}.\]

Then the variance of the Girard–Hutchinson estimator with Gaussian vectors x_i is

    \[\Var(\hat{\tr}_{\rm Gaussian}) = \frac{1}{m} \cdot 2 \sum_{i=1}^n \lambda_i^2.\]

For vectors x_i drawn from the sphere, we have

    \[\Var(\hat{\tr}_{\rm sphere}) = \frac{1}{m} \cdot \frac{n}{n+2} \cdot 2\sum_{i=1}^n (\lambda_i - \overline{\lambda})^2.\]

The sphere distribution improves on the Gaussian distribution in two ways. First, the variance of \Var(\hat{\tr}_{\rm sphere}) is smaller than \Var(\hat{\tr}_{\rm Gaussian})by a factor of n/(n+2) < 1. This improvement is quite minor. Second, and more importantly, \Var(\hat{\tr}_{\rm Gaussian}) is proportional to the sum of A‘s squared eigenvalues whereas \Var(\hat{\tr}_{\rm sphere}) is proportional to the sum of A‘s squared eigenvalues after having been shifted to be mean-zero!

The difference between Gaussian and sphere test vectors can be large. To see this, consider a 1000\times 1000 matrix A with eigenvalues uniformly distributed between 0.9 and 1.1 with a (Haar orthgonal) random matrix of eigenvectors. For simplicity, since the variance of all Girard–Hutchinson estimates is proportional to 1/m, we take m=1. Below show the variance of Girard–Hutchinson estimator for different distributions for the test vector. We see that the sphere distribution leads to a trace estimate which has a variance 300× smaller than the Gaussian distribution. For this example, the sphere and random sign distributions are similar.

DistributionVariance (divided by \tr(A)^2)
Gaussian2.0\times 10^{-3}
Sphere6.7\times 10^{-6}
Random signs6.7\times 10^{-6}

Which Distribution Should You Use: Signs vs. Sphere

The main point of this post is to argue against using the Gaussian distribution. But which distribution should you use: Random signs? The sphere distribution? The answer, for most applications, is one of those two, but exactly which depends on the properties of the matrix A.

The variance of the Girard–Hutchinson estimator with the random signs estimator is

    \[\Var(\hat{\tr}_{\rm signs}) = 2 \sum_{i\ne j} A_{ij}^2.\]

Thus, \Var(\hat{\tr}_{\rm signs}) depends on the size of the off-diagonal entries of A; \Var(\hat{\tr}_{\rm signs}) does not depend on the diagonal of A at all! For matrices with small off-diagonal entries (such as diagonally dominant matrices), the random signs distribution is often the best.

However, for other problems, the sphere distribution is preferable to random signs. The sphere distribution is rotation-invariant, so \Var(\hat{\tr}_{\rm sphere}) is independent of the eigenvectors of the (symmetric) matrix A, depending only on A‘s eigenvalues. By contrast, the variance of the Girard–Hutchinson estimator with the random signs distribution can significantly depend on the eigenvectors of the matrix A. For a given set of eigenvalues and the worst-case choice of eigenvectors, \Var(\hat{\tr}_{\rm sphere}) will always be smaller than \Var(\hat{\tr}_{\rm signs}). In fact, \Var(\hat{\tr}_{\rm sphere}) is the minimum variance distribution for Girard–Hutchinson trace estimation for a matrix with fixed eigenvalues and worst-case eigenvectors; see this section of my previous post for details.

In my experience, random signs and the sphere distribution are both perfectly adequate for trace estimation and either is a sensible default if you’re developing software. The Gaussian distribution on the other hand… don’t use it unless you have a good reason to.

How Good Can Stochastic Trace Estimates Be?

I am excited to share that our paper XTrace: Making the most of every sample in stochastic trace estimation has been published in the SIAM Journal on Matrix Analysis and Applications. (See also our paper on arXiv.)

Spurred by this exciting news, I wanted to take the opportunity to share one of my favorite results in randomized numerical linear algebra: a “speed limit” result of Meyer, Musco, Musco, and Woodruff that establishes a fundamental limitation on how accurate any trace estimation algorithm can be.

Let’s back up. Given an unknown square matrix A, the trace of A, defined to be the sum of its diagonal entries

    \[\tr(A) \coloneqq \sum_{i=1}^n A_{ii}.\]

The catch? We assume that we can only access the matrix A through matrix–vector products (affectionately known as “matvecs”): Given any vector x, we have access to Ax. Our goal is to form an estimate \hat{\tr} that is as accurate as possible while using as few matvecs as we can get away with.

To simplify things, let’s assume the matrix A is symmetric and positive (semi)definite. The classical algorithm for trace estimation is due to Girard and Hutchinson, producing a probabilistic estimate \hat{\tr} with a small average (relative) error:

    \[\expect\left[\frac{|\hat{\tr}-\tr(A)|}{\tr(A)}\right] \le \varepsilon \quad \text{using } m= \frac{\rm const}{\varepsilon^2} \text{ matvecs}.\]

If one wants high accuracy, this algorithm is expensive. To achieve just a 1% error (\varepsilon=0.01) requires roughly m=10,\!000 matvecs!

This state of affairs was greatly improved by Meyer, Musco, Musco, and Woodruff. Building upon previous work, they proposed the Hutch++ algorithm and proved it outputs an estimate \hat{\tr} satisfying the following bound:

(1)   \[\expect\left[\frac{|\hat{\tr}-\tr(A)|}{\tr(A)}\right] \le \varepsilon \quad \text{using } m= \frac{\rm const}{\varepsilon} \text{ matvecs}.\]

Now, we only require roughly m=100 matvecs to achieve 1% error! Our algorithm, XTrace, satisfies the same error guarantee (1) as Hutch++. On certain problems, XTrace can be quite a bit more accurate than Hutch++.

The MMMW Trace Estimation “Speed Limit”

Given the dramatic improvement of Hutch++ and XTrace over Girard–Hutchinson, it is natural to hope: Is there an algorithm that does even better than Hutch++ and XTrace? For instance, is there an algorithm satisfying an even slightly better error bound of the form

    \[\expect\left[\frac{|\hat{\tr}-\tr(A)|}{\tr(A)}\right] \le \varepsilon \quad \text{using } m= \frac{\rm const}{\varepsilon^{0.999}} \text{ matvecs}?\]

Unfortunately not. Hutch++ and XTrace are essentially as good as it gets.

Let’s add some fine print. Consider an algorithm for the trace estimation problem. Whenever the algorithm wants, it can present a vector x_i and receive back Ax_i. The algorithm is allowed to be adaptive: It can use the matvecs Ax_1,\ldots,Ax_s it has already collected to decide which vector x_{s+1} to present next. We measure the cost of the algorithm in terms of the number of matvecs alone, and the algorithm knows nothing about the psd matrix A other what it learns from matvecs.

One final stipulation:

Simple entries assumption. We assume that the entries of the vectors x_i presented by the algorithm are real numbers between -1 and 1 with up to b digits after the decimal place.

To get a feel for this simple entries assumption, suppose we set b=2. Then (-0.92,0.17) would be an allowed input vector, but (0.232,-0.125) would not be (too many digits after the decimal place). Similarly, (18.3,2.4) would not be valid because its entries exceed 1. The simple entries assumption is reasonable as we typically represent numbers on digital computers by storing a fixed number of digits of accuracy.1We typically represent numbers on digital computers by floating point numbers, which essentially represent numbers using scientific notation like 1.3278123 \times 10^{27}. For this analysis of trace estimation, we use fixed point numbers like 0.23218 (no powers of ten allowed)!

With all these stipulations, we are ready to state the “speed limit” for trace estimation proved by Meyer, Musco, Musco, and Woodruff:

Informal theorem (Meyer, Musco, Musco, Woodruff). Under the assumptions above, there is no trace estimation algorithm producing an estimate \hat{\tr} satisfying

    \[\expect\left[\frac{|\hat{\tr}-\tr(A)|}{\tr(A)}\right] \le \varepsilon \quad \text{using } m= \frac{\rm const}{\varepsilon^{0.999}} \text{ matvecs}.\]

We will see a slightly sharper version of the theorem below, but this statement captures the essence of the result.

Communication Complexity

To prove the MMMW theorem, we have to take a journey to the beautiful subject of communication complexity. The story is this. Alice and Bob are interested in solving a computational problem together. Alice has her input x and Bob has his input y, and they are interested in computing a function f(x,y) of both their inputs.

Unfortunately for the two of them, Alice and Bob are separated by a great distance, and can only communicate by sending single bits (0 or 1) of information over a slow network connection. Every bit of communication is costly. The field of communication complexity is dedicated to determining how efficiently Alice and Bob are able to solve problems of this form.

The Gap-Hamming problem is one example of a problem studied in communication complexity. As inputs, Alice and Bob receive vectors x,y \in \{\pm 1\}^n with +1 and -1 entries from a third party Eve. Eve promises Alice and Bob that their vectors x and y satisfy one of two conditions:

(2)   \[\text{Case 0: } x^\top y \ge\sqrt{n} \quad \text{or} \quad \text{Case 1: } x^\top y \le -\sqrt{n}. \]

Alice and Bob must work together, sending as few bits of communication as possible, to determine which case they are in.

There’s one simple solution to this problem: First, Bob sends his whole input vector y to Alice. Each entry of y takes one of the two value \pm 1 and can therefore be communicated in a single bit. Having received y, Alice computes x^\top y, determines whether they are in case 0 or case 1, and sends Bob a single bit to communicate the answer. This procedure requires n+1 bits of communication.

Can Alice and Bob still solve this problem with many fewer than n bits of communication, say \sqrt{n} bits? Unfortunately not. The following theorem of Chakrabati and Regev shows that roughly n bits of communication are needed to solve this problem:

Theorem (Chakrabati–Regev). Any algorithm which solves the Gap-Hamming problem that succeeds with at least 2/3 probability for every pair of inputs x and y (satisfying one of the conditions (2)) must take \Omega(n) bits of communication.

Here, \Omega(n) is big-Omega notation, closely related to big-O notation \order(n) and big-Theta notation \Theta(n). For the less familiar, it can be helpful to interpret \Omega(n), \order(n), and \Theta(n) as all standing for “proportional to n”. In plain language, the theorem of Chakrabati and Regev result states that there is no algorithm for the Gap-Hamming problem that much more effective than the basic algorithm where Bob sends his whole input to Alice (in the sense of requiring less than \order(n) bits of communication).

Reducing Gap-Hamming to Trace Estimation

This whole state of affairs is very sad for Alice and Bob, but what does it have to do with trace estimation? Remarkably, we can use hardness of the Gap-Hamming problem to show there’s no algorithm that fundamentally improves on Hutch++ and XTrace. The argument goes something like this:

  1. If there were a trace estimation algorithm fundamentally better than Hutch++ and XTrace, we could use it to solve Gap-Hamming in fewer than \order(n) bits of communication.
  2. But no algorithm can solve Gap-Hamming in fewer than \order(n) bits or communication.
  3. Therefore, no trace estimation algorithm is fundamentally better than Hutch++ and XTrace.

Step 2 is the work of Chakrabati and Regev, and step 3 follows logically from 1 and 2. Therefore, we are left to complete step 1 of the argument.

Protocol

Assume we have access to a really good trace estimation algorithm. We will use it to solve the Gap-Hamming problem. For simplicity, assume n is a perfect square. The basic idea is this:

  • Have Alice and Bob reshape their inputs x,y \in \{\pm 1\}^n into matrices X,Y\in\{\pm 1\}^{\sqrt{n}\times \sqrt{n}}, and consider (but do not form!) the positive semidefinite matrix

        \[A = (X+Y)^\top (X+Y).\]

  • Observe that

        \[\tr(A) = \tr(X^\top X) + 2\tr(X^\top Y) + \tr(Y^\top Y) = 2n + 2(x^\top y).\]

    Thus, the two cases in (2) can be equivalently written in terms of \tr(A):

    (2′)   \[\text{Case 0: } \tr(A)\ge 2n + 2\sqrt{n} \quad \text{or} \quad \text{Case 1: } \tr(A) \le 2n-2\sqrt{n}. \]

  • By working together, Alice and Bob can implement a trace estimation algorithm. Alice will be in charge of running the algorithm, but Alice and Bob must work together to compute matvecs. (Details below!)
  • Using the output of the trace estimation algorithm, Alice determines whether they are in case 0 or 1 (i.e., where \tr(A) \gg 2n or \tr(A) \ll 2n) and sends the result to Bob.

To complete this procedure, we just need to show how Alice and Bob can implement the matvec procedure using minimal communication. Suppose Alice and Bob want to compute Az for some vector z with entries between -1 and 1 with up to b decimal digits. First, convert z to a vector w\coloneqq 10^b z whose entries are integers between -10^b and 10^b. Since Az = 10^{-b}Aw, interconverting between Az and Aw is trivial. Alice and Bob’s procedure for computing Aw is as follows:

  • Alice sends Bob w.
  • Having received w, Bob forms Yw and sends it to Alice.
  • Having received Yw, Alice computes v\coloneqq Xw+Yw and sends it to Bob.
  • Having received v, Bob computes Y^\top v and sends its to Alice.
  • Alice forms Aw = X^\top v + Y^\top v.

Because X and Y are \sqrt{n}\times \sqrt{n} and have \pm 1 entries, all vectors computed in this procedure are vectors of length \sqrt{n} with integer entries between -4n 10^b and 4n10^b. We conclude the communication cost for one matvec is T\coloneqq\Theta((b+\log n)\sqrt{n}) bits.

Analysis

Consider an algorithm we’ll call BestTraceAlgorithm. Given any accuracy parameter \varepsilon > 0, BestTraceAlgorithm requires at most m = m(\varepsilon) matvecs and, for any positive semidefinite input matrix A of any size, produces an estimate \hat{\tr} satisfying

(3)   \[\expect\left[\frac{|\hat{\tr}-\tr(A)|}{\tr(A)}\right] \le \varepsilon.\]

We assume that BestTraceAlgorithm is the best possible algorithm in the sense that no algorithm can achieve (3) on all (positive semidefinite) inputs with m' < m matvecs.

To solve the Gap-Hamming problem, Alice and Bob just need enough accuracy in their trace estimation to distinguish between cases 0 and 1. In particular, if

    \[\left| \frac{\hat{\tr} - \tr(A)}{\tr(A)} \right| \le \frac{1}{\sqrt{n}},\]

then Alice and Bob can distinguish between cases 0 and 1 in (2′)

Suppose that Alice and Bob apply trace estimation to solve the Gap-Hamming problem, using m matvecs in total. The total communication is m\cdot T = \order(m(b+\log n)\sqrt{n}) bits. Chakrabati and Regev showed that Gap-Hamming requires cn bits of communication (for some c>0) to solve the Gap-Hamming problem with 2/3 probability. Thus, if m\cdot T < cn, then Alice and Bob fail to solve the Gap-Hamming problem with at least 1/3 probability. Thus,

    \[\text{If } m < \frac{cn}{T} = \Theta\left( \frac{\sqrt{n}}{b+\log n} \right), \quad \text{then } \left| \frac{\hat{\tr} - \tr(A)}{\tr(A)} \right| > \frac{1}{\sqrt{n}} \text{ with probability at least } \frac{1}{3}.\]

The contrapositive of this statement is that if

    \[\text{If }\left| \frac{\hat{\tr} - \tr(A)}{\tr(A)} \right| \le \frac{1}{\sqrt{n}}\text{ with probability at least } \frac{2}{3}, \quad \text{then } m \ge \Theta\left( \frac{\sqrt{n}}{b+\log n} \right).\]


Say Alice and Bob run BestTraceAlgorithm with parameter \varepsilon = \tfrac{1}{3\sqrt{n}}. Then, by (3) and Markov’s inequality,

    \[\left| \frac{\hat{\tr} - \tr(A)}{\tr(A)} \right| \le \frac{1}{\sqrt{n}} \quad \text{with probability at least }\frac{2}{3}.\]

Therefore, BestTraceAlgorithm requires at least

    \[m \ge \Theta\left( \frac{\sqrt{n}}{b+\log n} \right) \text{ matvecs}.\]

Using the fact that we’ve set \varepsilon = 1/3\sqrt{n}, we conclude that any trace estimation algorithm, even BestTraceAlgorithm, requires

    \[m \ge \Theta \left( \frac{1}{\varepsilon (b+\log(1/\varepsilon))} \right) \text{ matvecs}.\]

In particular, no trace estimation algorithm can achieve mean relative error \varepsilon using even \order(1/\varepsilon^{0.999}) matvecs. This proves the MMMW theorem.

Five Interpretations of Kernel Quadrature

I’m excited to share that my paper Kernel quadrature with randomly pivoted Cholesky, joint with Elvira Moreno, has been accepted to NeurIPS 2023 as a spotlight.

Today, I want to share with you a little about the kernel quadrature problem. To avoid this post getting too long, I’m going to write this post assuming familiarity with the concepts of reproducing kernel Hilbert spaces and Gaussian processes.

Integration and Quadrature

Integration is one of the most widely used operations in mathematics and its applications. As such, it is a basic problem of wide interest to develop numerical methods for evaluating integrals.

In this post, we will consider a quite general integration problem. Let \Omega\subseteq \real^d be a domain and let \mu be a (finite Borel) measure on \Omega. We consider the task of evaluating

    \[I[f] = \int_\Omega f(x) g(x) \, \mathrm{d}\mu(x).\]

One can imagine that g, \mu, and \Omega are fixed, but we may want to evaluate this same integral I[f] for multiple different functions f.

To evaluate, we will design a quadrature approximation to the integral I[f]:

    \[\hat{I}_{w,s}[f] = \sum_{i=1}^n w_i f(s_i) \approx I[f].\]

Concretely, we wish to find real numbers w = (w_1,\ldots,w_n) \in \real^n and points s = (s_1,\ldots,s_n) \in \Omega^n such that the approximation \hat{I}_{w,s}[f] \approx I[f] is accurate.

Smoothness and Reproducing Kernel Hilbert Spaces

As is frequently the case in computational mathematics, the accuracy we can expect for this integration problem depends on the smoothness of the integrand f. The more smooth f is, the more accurately we can expect to compute I[f] for a given budget of computational effort.

In this post, will measure smoothness using the reproducing kernel Hilbert space (RKHS) formalism. Let \mathcal{H} be an RKHS with norm \norm{\cdot}. We can interpret the norm as assigning a roughness \norm{f} to each function f. If \norm{f} is large, then f is rough; if \norm{f} is small, then f is smooth.

Associated to the RKHS \mathcal{H} is the titular reproducing kernel k. The kernel is a bivariate function k:\Omega\times\Omega\to\real. It is related to the RKHS inner product \langle\cdot,\cdot\rangle by the reproducing property

    \[f(x)=\langle f, k(x,\cdot)\rangle \quad \text{for every }f\in\mathcal{H},x\in\Omega.\]

Here, k(x,\cdot) represents the univariate function obtained by setting the first input of k to be x.

The Ideal Weights

To design a quadrature rule, we have to set the nodes s = (s_1,\ldots,s_n) \in \Omega^n and weights w = (w_1,\ldots,w_n)\in\real^n. Let’s first assume that the nodes s are fixed, and talk about how to pick the weights w.

There’s one choice of weights w^\star that we’ll called the ideal weights. There (at least) are five equivalent ways of characterizing the ideal weights. We’ll present all of them. As an exercise, you can try and convince yourself that these characterizations are equivalent, giving rise to the same weights.

Interpretation 1: Exactness

A standard way of designing quadrature rules is to make them exact (i.e., error-free) for some class of functions. For instance, many classical quadrature rules are exact for polynomials of degree up to n-1.

For kernel quadrature, it makes sense to design the quadrature rule to be exact for the kernel function at the selected nodes. That is, we require

    \[\hat{I}_{w_\star,s}[k(s_i,\cdot)]=I[k(s_i,\cdot)] \quad \text{for } i=1,2,\ldots,n.\]

Enforcing exactness gives us n linear equations for the n unknowns w^\star_1,\ldots,w^\star_n:

    \[\sum_{j=1}^n k(s_i,s_j)w^\star_j = \int_\Omega k(s_i,x) g(x)\,\mathrm{d}\mu(x) \quad \text{for }i=1,2,\ldots,n.\]

Under mild conditions, this system of linear equations is uniquely solvable, and the solution w^\star\in\real^n is the ideal weights.

Interpretation 2: Interpolate and Integrate

Here’s another very classical way of designing a quadrature rule. First, interpolate the function values (s_i,f(s_i)) at the nodes, obtaining an interpolant \hat{f}. Then, obtain an approximation to the integral by integrating the interpolant:

    \[\hat{I}_{w^\star,s}[f] \coloneqq \int_\Omega \hat{f}(x) g(x) \, \mathrm{d}\mu(x).\]


In our context, the appropriate interpolation method is kernel interpolation.1Kernel interpolation is also called Gaussian process regression or kriging though (confusingly) these terms can also refer to slightly different methods. It is the regularization-free limit of kernel ridge regression. The kernel interpolant is defined to be the minimum-norm function \hat{f} that interpolates the data:

    \[\hat{f} = \argmin \{ \norm{h} : h(s_i) = f(s_i) \text{ for } i=1,\ldots,n\}.\]

Remarkably, this infinite-dimensional problem has a tractably computable solution. In fact, \hat{f} is the unique function of the form

    \[\hat{f} = \sum_{i=1}^n \alpha_i k(\cdot,s_i)\]

that agrees with f on the points s_1,\ldots,s_n.With a little algebra, you can show that the integral of \hat{f} is

    \[I[\hat{f}] = \sum_{i=1}^n w^\star_i f(s_i),\]

where w^\star are the ideal weights.

Interpretation 3: Minimizing the Worst-Case Error

Define the worst-case error of weights w and nodes s to be

    \[\operatorname{Err}(w,s)=\sup_{\norm{f}\le 1}\left| I[f] - \hat{I}_{w,s}[f]\right|.\]

The quantity \operatorname{Err}(w,s) is the highest possible quadrature error for a function f\in\mathcal{H} of norm at most 1.

Having defined the worst-case error, the ideal weights are precisely the weights that minimize this quantity

    \[w^\star=\operatorname*{argmin}_{w\in\real^n}\operatorname{Err}(w,s).\]

Interpretation 4: Minimizing the Mean-Square Error

The next two interpretations of the ideal weights will adopt a probabilistic framing. A Gaussian process is a random function f such that f’s values at any collection of points are (jointly) Gaussian random variables. We write f\sim \operatorname{GP}(0,k) for a mean-zero Gaussian process with covariance function k:

    \[\Cov(f(x),f(y))=k(x,y)\quad \text{for every } x,y\in\Omega.\]


Define the mean-square quadrature error of weights w and nodes s to be

    \[\operatorname{MSE}(w,s)\coloneqq \expect_{f\sim\operatorname{GP}(0,k)} \left( I[f] - \hat{I}_{w,s}[f] \right)^2.\]

The mean-square error reports the expected squared quadrature error over all functions f drawn from a Gaussian process with covariance function k.

Pleasantly, the mean-square error is equal ro the square of the worst-case error

    \[\operatorname{MSE}(w,s)=\operatorname{Err}(w,s)^2.\]

As such, the ideal weights also minimize the mean-square error

    \[w^\star=\operatorname*{argmin}_{w\in\real^n}\operatorname{MSE}(w,s).\]

Interpretation 5: Conditional Expectation

For our last interpretation, again consider a Gaussian process h\sim \operatorname{GP}(0,k). The integral of this random function I[h] is a random variable. To numerically integrate a function f, compute the expectation of I[h] conditional on h agreeing with f at the quadrature nodes:

    \[\hat{I}_{w^\star,s}[f]\coloneqq \expect_{h\sim\operatorname{GP}(0,k)}[I[h] \mid h(s_i)=f(s_i) \text{ for } i=1,\ldots,n].\]

One can show that this procedure yields the quadrature scheme with the ideal weights.

Conclusion

We’ve just seen five sensible ways of defining the ideal weights for quadrature in a general reproducing kernel Hilbert space. Remarkably, all five lead to exactly the same choice of weights. To me, these five equivalent characterizations give me more confidence that the ideal weights really are the “right” or “natural” choice for kernel quadrature.

That said, there are other reasonable requirements that we might want to impose on the weights. For instance, if \mu is a probability measure and g\equiv 1, it is reasonable to add an additional constraint that the weights w lie in the probability simplex

    \[w\in\Delta\coloneqq \left\{ p\in\real^n_+ : \sum_{i=1}^n p_i = 1\right\}.\]

With this additional stipulation, a quadrature rule can be interpreted as integrating f against a discrete probability measure \ \hat{\mu}=\sum_{i=1}^n w_i\delta_{s_i}; thus, in effect, quadrature amounts to approximating one probability measure \mu by another \hat{\mu}. Additional constraints such as these can easily be imposed when using the optimization characterizations 3 and 4 of the ideal weights. See this paper for details.

What About the Nodes?

We’ve spent a lot of time talking about how to pick the quadrature weights, but how should we pick the nodes s\in\Omega^n? To pick the nodes, it seems sensible to try and minimize the worst-case error \operatorname{Err}(w^\star,s) with the ideal weights w^\star. For this purpose, we can use the following formula:

    \[\operatorname{Err}(w^\star,s) = \norm{\int_\Omega (k(\cdot,x) - \hat{k}_s(\cdot,x)) g(x) \, \mathrm{d}\mu(x)}.\]

Here, \hat{k}_s is the Nyström approximation to the kernel k induced by the nodes s, defined to be

    \[\hat{k}_s(x,y) = k(x,s) k(s,s)^{-1} k(s,y).\]

We have written k(s,s) for the kernel matrix with ij entry k(s_i,s_j) and k(x,s) and k(s,y) for the row and column vectors with ith entry k(x,s_i) and k(s_i,y).

I find the appearance of the Nyström approximation in this context to be surprising and delightful. Previously on this blog, we’ve seen (column) Nyström approximation in the context of matrix low-rank approximation. Now, a continuum analog of the matrix Nyström approximation has appeared in the error formula for numerical integration.

The appearance of the Nyström approximation in the kernel quadrature error \operatorname{Err}(w^\star,s) also suggests a strategy for picking the nodes.

Node selection strategy. We should pick the nodes s to make the Nyström approximation \hat{k}_s \approx k as accurate as possible.

The closer \hat{k}_s is to k, the smaller the function k(\cdot,x) - \hat{k}_s(\cdot,x) is and, thus, the smaller the error

    \[\operatorname{Err}(w^\star,s) = \norm{\int_\Omega (k(\cdot,x) - \hat{k}_s(\cdot,x)) g(x) \, \mathrm{d}\mu(x)}.\]

Fortunately, we have randomized matrix algorithms for picking good nodes for matrix Nyström approximation such as randomly pivoted Cholesky, ridge leverage score sampling, and determinantal point process sampling; maybe these matrix tools can be ported to the continuous kernel setting?

Indeed, all three of these algorithms—randomly pivoted Cholesky, ridge leverage score sampling, and determinantal point process sampling—have been studied for kernel quadrature. The first of these algorithms, randomly pivoted Cholesky, is the subject of our paper. We show that this simple, adaptive sampling method produces excellent nodes for kernel quadrature. Intuitively, randomly pivoted Cholesky is effective because it is repulsive: After having picked nodes s_1,\ldots,s_i, it has a high probability of placing the next node s_{i+1} far from the previously selected nodes.

The following image shows 20 nodes selected by randomly pivoted Cholesky in a crescent-shaped region. The cyan–pink shading denotes the probability distribution for picking the next node. We see that the center of the crescent does not have any nodes, and thus is most likely to receive a node during the next round of sampling.

In our paper, we demonstrate—empirically and theoretically—that randomly pivoted Cholesky produces excellent nodes for quadrature. We also discuss efficient rejection sampling algorithms for sampling nodes with the randomly pivoted Cholesky distribution. Check out the paper for details!