Perron-Frobenius Contractive Operator Matching for Data-Driven Reachable Fault Identification and Recovery

TL;DR

This paper introduces a novel data-driven framework using Perron-Frobenius operators in probability density space for fault detection, identification, and recovery in nonlinear control systems, validated on spacecraft attitude control.

Contribution

It develops a unified density-based approach with learned operators and certifiable bounds for fault detection and recovery, advancing beyond trajectory-based methods.

Findings

Accurately predicts fault-induced density evolution.

Provides certifiable bounds for fault detectability.

Demonstrates effectiveness on spacecraft control system.

Abstract

This paper focuses on data-driven fault detection, identification, and recovery (FDIR) for nonlinear control-affine systems under actuator faults. We create a unified framework in the space of probability densities, rather than on individual trajectories, using fault-indexed Perron--Frobenius (PF) operators to predict the evolution of state distributions under different fault profiles. By leveraging the probability-flow representation of the Fokker--Planck equation, we construct deterministic PF operators that reproduce exact stochastic marginals, define forward reachable density families, and establish certifiable 2-Wasserstein bounds on the divergence between fault-driven and nominal density evolutions. These provide quantitative conditions for the detectability and identifiability of various faults. The fault-indexed operators are learned from trajectory data via flow map matching (FMM), and we demonstrate that the observable FMM residual directly bounds the approximation error of the operator in the 2-Wasserstein metric. Additionally, we co-train a contraction certificate that bounds the gap between the learned operator family, the actual fault-driven density flow, and the nominal dynamics. The operator library is then used online for continuous fault parameter fitting over a continuous parameter space to generalize the learned operators to out-of-distribution (OOD) scenarios. To carry out the recovery control, we employ reachable density propagation and Gaussian mixture covariance steering. The proposed framework is validated on a 10-state spacecraft attitude-control system with four reaction wheels.