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Advanced Modeling and Dynamic Stability Analysis of the Aerodynamic Control Surfaces of CALLISTO

Briese, Lale Evrim and Kier, Thiemo and Petkov, Ivaylo and Windelberg, Jens and Heinrich, Lars and Krummen, Sven (2023) Advanced Modeling and Dynamic Stability Analysis of the Aerodynamic Control Surfaces of CALLISTO. In: AIAA SciTech 2023 Forum. AIAA SciTech Forum, 2023-01-23 - 2023-01-27, National Harbor, USA. doi: 10.2514/6.2023-2405.

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Abstract

In order to assess future reusable launch vehicle concepts and their key technologies, the Centre National d'Etudes Spatiales (CNES), the Japan Aerospace Exploration Agency (JAXA), and the German Aerospace Center (DLR) are currently developing a vertical take-off vertical landing reusable launch vehicle demonstrator within the trilateral project CALLISTO. For attitude control during descent, aerodynamic control surfaces are used, which can be exposed to significant unsteady aerodynamic loads. Therefore, the aerodynamic control surfaces must be designed to avoid any unstable behavior related to a coupling between structural deformation and aerodynamic flow in conjunction with the servo-loop. For this purpose, dynamic stability studies have been performed using a condensed Finite Element model to represent the structural dynamics and the Doublet Lattice Method to compute the unsteady aerodynamics within the subsonic flight regime. The time-domain integration of the unsteady aerodynamic matrices is performed by Rational Function Approximation, which are then used to obtain state-space matrices based on the p-method for each flight condition. By evaluating the eigenvalues of the state-space matrices, the dynamic stability behavior is assessed. The objective of this paper is to present the modeling strategy and systematic assessment of the dynamic stability behavior of CALLISTO's aerodynamic control surfaces.

Item URL in elib:https://elib.dlr.de/193834/
Document Type:Conference or Workshop Item (Speech)
Title:Advanced Modeling and Dynamic Stability Analysis of the Aerodynamic Control Surfaces of CALLISTO
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Briese, Lale EvrimUNSPECIFIEDhttps://orcid.org/0000-0003-0900-2005UNSPECIFIED
Kier, ThiemoUNSPECIFIEDhttps://orcid.org/0000-0002-6210-6295UNSPECIFIED
Petkov, IvayloUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Windelberg, JensUNSPECIFIEDhttps://orcid.org/0000-0002-9249-2967UNSPECIFIED
Heinrich, LarsUNSPECIFIEDhttps://orcid.org/0000-0003-4796-5021UNSPECIFIED
Krummen, SvenUNSPECIFIEDhttps://orcid.org/0000-0002-4126-688XUNSPECIFIED
Date:January 2023
Journal or Publication Title:AIAA SciTech 2023 Forum
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
DOI:10.2514/6.2023-2405
Status:Published
Keywords:dynamic stability, flutter, aeroservoelasticity, reusable launch vehicle, VTVL, aerodynamic control surface, CALLISTO
Event Title:AIAA SciTech Forum
Event Location:National Harbor, USA
Event Type:international Conference
Event Start Date:23 January 2023
Event End Date:27 January 2023
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Space
HGF - Program Themes:Space Transportation
DLR - Research area:Raumfahrt
DLR - Program:R RP - Space Transportation
DLR - Research theme (Project):R - Project CALLISTO [RP]
Location: Oberpfaffenhofen
Institutes and Institutions:Institute of System Dynamics and Control > Space System Dynamics
Institute of System Dynamics and Control > Aircraft System Dynamics
Institute of Structures and Design > Space System Integration
Institute of Flight Systems > Safety Critical Systems&Systems Engineering
Institut für Systemleichtbau > Composite Design
Institute of Space Systems > Systems Engineering and Project Office
Deposited By: Briese, Lale Evrim
Deposited On:12 Sep 2023 09:03
Last Modified:24 Apr 2024 20:54

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