Unverified 2026

Adaptive Sliding-Mode Disturbance-Observer Optimizer

Implementation & benchmark of arXiv:2607.27524 — Estimated-State Adaptive Sliding Mode Control and Disturbance Observation Using Second-Order Surfaces for Spacecraft Formation Reconfiguration

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Source paper: Estimated-State Adaptive Sliding Mode Control and Disturbance Observation Using Second-Order Surfaces for Spacecraft Formation Reconfiguration arXiv:2607.27524 ⓘ · analyzed Aug 31, 2026

AI-generated research hypothesis, automatically tested. Not peer-reviewed.

Idea description

Replace a conventional momentum update by a second-order optimization state with an adaptive robust correction. An online disturbance observer estimates the difference between intended gradient-driven dynamics and observed optimizer dynamics, while an adaptive sliding gain compensates for the remaining bounded disturbance. This is intended for minibatch noise, stale gradients, curvature variation, or gradient compression that produces intermittent optimizer instability.

Formulas

theta_dot = v, tau v_dot = -v - g(theta) + u + d(t), g(theta) = gradient of L(theta)
s = v + alpha g(theta), d_hat_dot = ell sat(s / epsilon), u = -d_hat - k sat(s / epsilon)
k_dot = gamma norm(s) - sigma (k - k0), r = d - d_hat, norm(r) <= Delta implies d(norm(s))/dt approximately <= -(k - Delta)/tau
norm(s) approximately <= epsilon + Delta/k; robust contraction is expected when k > Delta

Mathematical statement

Let theta be the parameter vector, v the optimizer velocity, g(theta) the minibatch gradient, alpha positive the sliding-surface coefficient, tau positive the optimizer time constant, and d(t) an unknown disturbance representing stochastic-gradient error and unmodeled curvature. Use the artificial second-order dynamics theta_dot = v and tau v_dot = -v - g(theta) + u + d(t). Define the sliding variable s = v + alpha g(theta). Estimate the disturbance using d_hat_dot = ell sat(s / epsilon), where ell is an observer gain and epsilon is a boundary-layer width. Apply u = -d_hat - k sat(s / epsilon), where k is an adaptive gain. Update k using k_dot = gamma times the norm of s minus sigma times (k - k0). If the residual r = d - d_hat is bounded by Delta, then outside the boundary layer the robust term dominates when k exceeds Delta, giving approximately d(norm(s))/dt <= -(k - Delta)/tau. The practical sliding error should therefore scale as epsilon + Delta/k.

Implementation notes

Integrate the method at the optimizer level, not inside individual neural-network layers. Maintain the parameter vector theta, velocity v, disturbance estimate d_hat, and adaptive gain k for each parameter group or for the entire model. At every minibatch, compute the ordinary gradient g. Form s = v + alpha times g, which avoids a Hessian-vector product and avoids finite-difference differentiation. Compute z = s divided by epsilon and use sat(z) = z divided by max(1, norm(z)) for groupwise vector saturation. Update d_hat by d_hat <- d_hat + eta_obs times ell times sat(z), then compute robust <- -d_hat - k times sat(z). Apply the discrete dynamics v <- beta v - eta g + eta robust and theta <- theta + v, with beta chosen near 1 - eta/tau. Update k by k <- max(k_min, k + eta times (gamma norm(s) - sigma(k-k0))). Clip d_hat and k only for numerical safety, while logging their unclipped values. The paper-derived mechanism is the observer, sliding surface, adaptive gain, and residual-dominance condition; Delta must be estimated empirically from the norm of observed minibatch or update mismatch. First test a two-layer MLP on MNIST, comparing SGD with momentum, Adam, and this optimizer at matched learning-rate budgets for batch sizes 32 and 512, with and without deliberately injected gradient noise. Measure the largest stable learning rate and log norm(s), k, d_hat, and update norms. The predicted signature is that divergence should disappear after the steady gain crosses the measured disturbance scale Delta. The median sliding error should decrease approximately as 1/k until reaching an epsilon-dependent floor. Estimate the empirical threshold k_c from the point where the slope of log(norm(s)) becomes negative; the prediction is k_c approximately equal to Delta within 20 percent. Increasing epsilon should increase the final error floor approximately proportionally, while increasing k above k_c should not significantly improve error below that floor.

Verification

This idea has not been verified yet.

Verification happens in two stages: Stage 1 — a mechanism check on a toy system confirms the claimed mathematical phenomenon reproduces; Stage 2 — a benchmark implements the idea on a real (small) neural network task and compares it against a tuned baseline over 8 paired seeds with a permutation test.

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