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Robust Performance Analysis for Gust Loads Computation

Knoblach, Andreas (2015) Robust Performance Analysis for Gust Loads Computation. Dissertation, Technische Universität Hamburg.

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Official URL: http://www.dr.hut-verlag.de/978-3-8439-2251-7.html

Abstract

In the design process of modern aircraft, a comprehensive analysis of worst case structural gust loads is imperative. Because this analysis requires to consider millions of cases, the examination is extremely time consuming. To solve this problem, a new approach based on robust performance analysis is introduced: the worst case energy-to-peak gain is used to efficiently determine worst case loads of nominal, uncertain, and linear parameter varying gust loads models.

Item URL in elib:https://elib.dlr.de/98482/
Document Type:Thesis (Dissertation)
Title:Robust Performance Analysis for Gust Loads Computation
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Knoblach, AndreasAndreas.Knoblach (at) DLR.deUNSPECIFIED
Date:July 2015
Refereed publication:Yes
Open Access:Yes
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Number of Pages:149
Status:Published
Keywords:gust loads, flexible aircraft, robust control theory, energy-to-peak gain
Institution:Technische Universität Hamburg
Department:Institute of Control Systems
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Aeronautics
HGF - Program Themes:fixed-wing aircraft
DLR - Research area:Aeronautics
DLR - Program:L AR - Aircraft Research
DLR - Research theme (Project):L - Systems and Cabin
Location: Oberpfaffenhofen
Institutes and Institutions:Institute of System Dynamics and Control > Aircraft System Dynamics
Deposited By: Knoblach, Andreas
Deposited On:30 Oct 2015 17:24
Last Modified:31 Jul 2019 19:55

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