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Nathaniel Mailhot

Publications and source records attributed to Nathaniel Mailhot.

2 recordsLinked to original sources

Approximate Dynamic Programming for Link Reconfiguration to Reduce Malicious Input Controllability in Consensus Networks

Communication links influence how strongly a malicious input at one sensor affects a consensus network. We study how a defender can reduce this influence by selecting one additional link after observing the currently attacked sensor. The attacked sensor changes over time, and vulnerability is measured by the trace of a finite-horizon controllability Gramian. A prescribed local epsilon-greedy attacker response rule defines a discounted Markov decision process for the defender. Exact dynamic programming (DP) provides an optimal policy using the full Gramian payoff matrix and attacker transition model. We then introduce approximate dynamic programming (ADP) that learns from sampled attacker transitions and empirical Gramian costs estimated from measured impulse responses. Under conditionally unbiased costs and standard sampling and learning-rate conditions, the learned action-value table converges to the exact DP solution. The analysis uses Bellman contraction and bounds the effect of persistent Gramian estimation bias, establishing when measured responses recover optimal defender decisions without constructing the full payoff matrix. In simulations on 20- and 100-node graphs, empirical ADP rollout costs are within 0.23% and 1.76%, respectively, of exact DP. In a two-dimensional intruder tracking example, both policies reduce network-wide root-mean-square tracking error spread by approximately 25% relative to an unmitigated attack.

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Guidance Mechanism for Flexible Wing Aircraft Using Measurement-Interfaced Machine Learning Platform

The autonomous operation of flexible-wing aircraft is technically challenging and has never been presented within literature. The lack of an exact modeling framework is due to the complex nonlinear aerodynamic relationships governed by the deformations in the flexible-wing shape, which in turn complicates the controls and instrumentation setup of the navigation system. This urged for innovative approaches to interface affordable instrumentation platforms to autonomously control this type of aircraft. This work leverages ideas from instrumentation and measurements, machine learning, and optimization fields in order to develop an autonomous navigation system for a flexible-wing aircraft. A novel machine learning process based on a guiding search mechanism is developed to interface real-time measurements of wing-orientation dynamics into control decisions. This process is realized using an online value iteration algorithm that decides on two improved and interacting model-free control strategies in real-time. The first strategy is concerned with achieving the tracking objectives while the second supports the stability of the system. A neural network platform that employs adaptive critics is utilized to approximate the control strategies while approximating the assessments of their values. An experimental actuation system is utilized to test the validity of the proposed platform. The experimental results are shown to be aligned with the stability features of the proposed model-free adaptive learning approach.

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