✗ Mechanism failed 2026

Time-Delay Error Adaptive Optimizer

Implementation & benchmark of arXiv:2608.10770 — Variable-Step Time-Delay Control for Proactive Aperiodic Spacecraft Attitude Control

Usefulness7/10
Difficulty5/10
Novelty7/10

Source paper: Variable-Step Time-Delay Control for Proactive Aperiodic Spacecraft Attitude Control arXiv:2608.10770 ⓘ · analyzed Sep 1, 2026

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 Not peer-reviewed.

Idea description

Treat minibatch optimizer steps as sampled control actions and adapt the next effective update interval from the discrepancy between a current-gradient realization and a delayed or extrapolated gradient. Use the quadratic time-delay-error mechanism to increase the interval in locally smooth regions and shrink it near curvature changes, while clipping both the interval and its ratio to prevent unstable jumps.

Formulas

$$\|\mathrm{TDE}_k\|\le C h_k^2,$$
$$r_k=g_k-\widehat g_k,\qquad \widehat g_k=g_{k-1}+\frac{h_k}{h_{k-1}}(g_{k-1}-g_{k-2}),$$
$$h_{k+1}=\operatorname{clip}_{[h_{\min},h_{\max}]\cap[h_k/q,qh_k]}\left(\sqrt{\frac{\varepsilon}{\|r_k\|_2+\delta}}\right),$$
$$\|r_k\|_2\approx C h_k^2\quad\Longrightarrow\quad h^*\approx\sqrt{\frac{\varepsilon}{C}}.$$

Mathematical statement

Let $w(t)\in\mathbb{R}^p$ be neural-network parameters, $g_k=\nabla L(w_k,\xi_k)$ the stochastic gradient at update $k$, and $h_k=t_{k+1}-t_k$ the effective optimizer interval. The transferable structural claim is that the system time-delay error obeys $\|\mathrm{TDE}_k\|\le C h_k^2$ for bounded local variation, where $C>0$ summarizes unknown dynamics and uncertainty. Define the optimizer residual $r_k=g_k-\widehat g_k$, with $\widehat g_k$ a gradient extrapolated from previous updates. Choose the next interval from the residual tolerance $\varepsilon$ using a square-root law. Here $h_{\min}$ and $h_{\max}$ are hard interval bounds, $q\ge1$ is the maximum allowed step ratio, and $\delta>0$ prevents division by zero. If $\|r_k\|\approx C h_k^2$, the target interval is $h^*\approx\sqrt{\varepsilon/C}$.

Implementation notes

1. Integration point: implement this as a wrapper around SGD or momentum SGD, initially avoiding Adam's internal normalization so that the meaning of the interval is clear. Interpret $h_k$ as the multiplier of the proposed parameter displacement: compute a direction $d_k$ and update $w_{k+1}=w_k-h_kd_k$. Store the last three gradients, their intervals, and the last residual. A fixed probe minibatch can be used to reduce measurement noise while training gradients remain stochastic. 2. Pseudocode: compute $g_k$ and the base optimizer direction $d_k$; form $\widehat g_k=g_{k-1}+(h_k/h_{k-1})(g_{k-1}-g_{k-2})$; calculate $r_k=g_k-\widehat g_k$; compute $h_{\mathrm{raw}}=\sqrt{\varepsilon/(\|r_k\|_2+\delta)}$; project it onto $[h_{\min},h_{\max}]$ and then onto $[h_k/q,qh_k]$; apply $w\leftarrow w-h_kd_k$. For noisy minibatches, use $R_k=\beta R_{k-1}+(1-\beta)\|r_k\|_2$ and substitute $R_k$ for the raw norm. Initialize with three fixed-step updates. 3. Taken from the paper: quadratic error scaling, the algebraic square-root scheduler, and bounded step-ratio design. Estimated empirically: $C$, residual noise, and the useful tolerance $\varepsilon$. 4. First experiment: train a two-layer MLP on MNIST with full-batch or large-batch SGD, comparing fixed-step SGD, cosine scheduling, and this scheduler at matched average step size. Sweep fixed $h$ values and measure residual norm versus $h$; fit a log-log slope. The quantitative prediction is a slope of approximately $2\pm0.3$ in the smooth full-batch regime, a stable operating interval near $h^*=\sqrt{\varepsilon/C}$, and bounded ratios $h_{k+1}/h_k\in[1/q,q]$. Test whether the residual settles within 20 percent of $\varepsilon$ and whether adaptive shortening precedes loss spikes when the fixed-step baseline crosses its divergence boundary.

Verification

Mechanism failed

Stage 1 · Toy mechanism gate: Failed ✗

Stage 2 · Mechanism transferred to benchmark: Not tested

Stage 2 · Practical benchmark result: Not run

Methodology: Toy-system gate first; the benchmark stage runs only after a pass. How verification works

Stage 1 — Mechanism check agent confidence 9/10

Built and ran a deterministic toy verification plus a CUDA PyTorch SGD/MLP comparison. The quadratic residual prediction was confirmed exactly (observed log-log slope 2.0000 versus predicted 2.0), and interval ratios respected [1/1.35, 1.35]. However, the stated absolute update h_next=sqrt(epsilon/||r||) does not converge to the claimed sqrt(epsilon/C) target when ||r||=C h^2: it converged to 0.3758 versus the claimed 0.1387, matching the fourth-root fixed point 0.3724. The adaptive benchmark had slightly lower final loss than fixed SGD but essentially identical accuracy, so the strict mechanism criterion fails.

Agent confidence
9/10
Baseline
Fixed SGD: final loss 0.07088, accuracy 0.96971, mean interval 0.0800.
Idea
Adaptive SGD: final loss 0.06977, accuracy 0.96975, mean interval 0.13217, interval range [0.0800, 0.1793]. Toy slope: observed 2.0000 versus predicted 2.0; observed scheduler interval 0.37582; claimed square-root target 0.13868; fourth-root fixed point 0.37239.

Limitations: Only a small synthetic two-class MLP was tested, not MNIST or larger networks. No matched-FLOP study, divergence-boundary sweep, multiple-seed statistics, or direct noisy-gradient residual-to-tolerance analysis was performed. CUDA fallback is handled for runtime errors, but the reported run used CUDA.

How to run: python3 experiment.py

Verdict computed by deterministic test code from paired-seed statistics — not by the language model.

Artifacts

Implementation overview ⬇ Download all as ZIP 3 files · code, reports and structured results