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Probabilistic Robustness Analysis with Aerospace Applications

Evangelisti, Luca (2023) Probabilistic Robustness Analysis with Aerospace Applications. Dissertation, Technische Universität Dresden.

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Official URL: https://nbn-resolving.org/urn:nbn:de:bsz:14-qucosa2-881689

Abstract

This thesis develops theoretical and computational methods for the robustness analysis of uncertain systems. The considered systems are linearized and depend rationally on random parameters with an associated probability distribution. The uncertainty is tackled by applying a polynomial chaos expansion (PCE), a series expansion for random variables similar to the well-known Fourier series for periodic time signals. We consider the linear perturbations around a system's operating point, i.e., reference trajectory, both from a probabilistic and worst-case point of view. A chief contribution is the polynomial chaos series expansion of uncertain linear systems in linear fractional representation (LFR). This leads to significant computational benefits when analyzing the probabilistic perturbations around a system's reference trajectory. The series expansion of uncertain interconnections in LFR further delivers important theoretical insights. For instance, it is shown that the PCE of rational parameter-dependent linear systems in LFR is equivalent to applying Gaussian quadrature for numerical integration. We further approximate the worst-case performance of uncertain linear systems with respect to quadratic performance metrics. This is achieved by approximately solving the underlying parametric Riccati differential equation after applying a polynomial chaos series expansion. The utility of the proposed probabilistic robustness analysis is demonstrated on the example of an industry-sized autolanding system for an Airbus A330 aircraft. Mean and standard deviation of the stochastic perturbations are quantified efficiently by applying a PCE to a linearization of the system along the nominal approach trajectory. Random uncertainty in the aerodynamic coefficients and mass parameters are considered, as well as atmospheric turbulence and static wind shear. The approximate worst-case analysis is compared with Monte Carlo simulations of the complete nonlinear model. The methods proposed throughout the thesis rapidly provide analysis results in good agreement with the Monte Carlo benchmark, at reduced computational cost.

Item URL in elib:https://elib.dlr.de/202032/
Document Type:Thesis (Dissertation)
Title:Probabilistic Robustness Analysis with Aerospace Applications
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Evangelisti, LucaLuca.Evangelisti (at) dlr.deUNSPECIFIEDUNSPECIFIED
Date:23 October 2023
Refereed publication:Yes
Open Access:No
Status:Published
Keywords:Robust Control, Polynomial Chaos Series Expansion, Linear Fractional Transformation, Gaussian Quadrature, Aircraft Automatic Landing
Institution:Technische Universität Dresden
Department:Professur für Flugmechanik und Flugregelung
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Aeronautics
HGF - Program Themes:Components and Systems
DLR - Research area:Aeronautics
DLR - Program:L CS - Components and Systems
DLR - Research theme (Project):L - Aircraft Systems
Location: Oberpfaffenhofen
Institutes and Institutions:Institute of System Dynamics and Control > Aircraft System Dynamics
Deposited By: Looye, Dr. Gertjan
Deposited On:15 Jan 2024 09:14
Last Modified:15 Jan 2024 09:14

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