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Methodical Coupling of Multidisciplinary Structural Design and Flight Control Systems

Nussbächer, Daniel Frank (2025) Methodical Coupling of Multidisciplinary Structural Design and Flight Control Systems. Dissertation, Technische Universität München.

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Official URL: https://nbn-resolving.org/urn:nbn:de:bvb:91-diss-20251110-1765864-0-4

Abstract

In integrated airframe design, respecting actively controlled effects is not as well established as taking passive phenomena into account. Unused potentials can be tapped if the process is extended by active components. Aeroservoelastic optimisation procedures are developed and realised through numerical programming. Their application in different studies shows that the tapped potentials must not remain unused for modern aircraft design.

Item URL in elib:https://elib.dlr.de/222246/
Document Type:Thesis (Dissertation)
Title:Methodical Coupling of Multidisciplinary Structural Design and Flight Control Systems
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Nussbächer, Daniel FrankTechnische Universität MünchenUNSPECIFIEDUNSPECIFIED
DLR Supervisors:
ContributionDLR SupervisorInstitution or E-MailDLR Supervisor's ORCID iD
Thesis advisorKrüger, Wolf R.Wolf.Krueger (at) dlr.dehttps://orcid.org/0000-0002-7949-1169
Date:December 2025
Open Access:No
Number of Pages:187
Status:Published
Keywords:aircraft design, preliminary structural design, optimization, flight control
Institution:Technische Universität München
Department:TUM School of Engineering and Design
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Aeronautics
HGF - Program Themes:Efficient Vehicle
DLR - Research area:Aeronautics
DLR - Program:L EV - Efficient Vehicle
DLR - Research theme (Project):L - Virtual Aircraft and  Validation
Location: Göttingen
Institutes and Institutions:Institute of Aeroelasticity > Loads Analysis and Aeroelastic Design
Deposited By: Krüger, Prof. Dr.-Ing. Wolf R.
Deposited On:20 Jan 2026 12:02
Last Modified:20 Jan 2026 12:02

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