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Maria Prandini

Researcher at Polytechnic University of Milan

Publications -  219
Citations -  4710

Maria Prandini is an academic researcher from Polytechnic University of Milan. The author has contributed to research in topics: Probabilistic logic & Optimization problem. The author has an hindex of 29, co-authored 212 publications receiving 4032 citations. Previous affiliations of Maria Prandini include University of Oxford & Brescia University.

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Probabilistic reachability and safety for controlled discrete time stochastic hybrid systems

TL;DR: In this work, probabilistic reachability over a finite horizon is investigated for a class of discrete time stochastic hybrid systems with control inputs and it is revealed that it is amenable to two complementary interpretations, leading to dual algorithms for reachability computations.
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The scenario approach for systems and control design

TL;DR: The scenario approach is illustrated at a tutorial level, focusing mainly on algorithmic aspects, and its versatility and virtues will be pointed out through a number of examples in model reduction, robust and optimal control.
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A probabilistic approach to aircraft conflict detection

TL;DR: An algorithm for decentralized conflict detection and resolution that generalizes potential fields methods for path planning to a probabilistic dynamic environment is proposed and validated using Monte Carlo simulations.
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Approximate Model Checking of Stochastic Hybrid Systems

TL;DR: Under certain regularity conditions on the transition and reset kernels governing the dynamics of the stochastic hybrid system, the invariance probability computed using the approximating Markov chain is shown to converge to the invariant probability of the original stochastics hybrid system as the grid used in the approximation gets finer.
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Optimal coordinated maneuvers for three dimensional aircraft conflict resolution

TL;DR: In this article, an energy function was proposed to select among all the conflict-free maneuvers the optimal one, and a geometric construction and a numerical algorithm for computing the optimal resolution maneuvers were given in the two aircraft case.