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The Space Liner Federation - Distributed Space Vehicle Simulation Based on Loose Coupling

Morlang, Frank und Strassburger, Steffen (2024) The Space Liner Federation - Distributed Space Vehicle Simulation Based on Loose Coupling. In: 2024 IEEE Aerospace Conference, AERO 2024. 2024 IEEE Aerospace Conference, 2024-03-02 - 2024-03-09, Big Sky, MT, USA. doi: 10.1109/AERO58975.2024.10521195. ISBN 979-835030462-6. ISSN 1095-323X.

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Offizielle URL: https://ieeexplore.ieee.org/document/10521195

Kurzfassung

This paper describes a Web Live, Virtual, Constructive server approach that provides compliancy to the future High Level Architecture distributed simulation standard called "HLA 4", currently in the final balloting process at IEEE but not yet released. It represents a sustainable, alternative approach to already start with, being HLA 4 compliant as soon as this new standard will be released. The communication between loosely coupled web simulation modules and the run-time infrastructure of the future HLA standard is realized by service bridging from the Web Live, Virtual, Constructive protocol over WebSockets. This will enhance interoperability and re-use potential, because web simulation module developers do not have to cope with the specifics of HLA and can use the web standards they are experienced with. Although developed in a scripting language, an own server software development covers this bridging task. Its performance results from the use of a set of extension packages, providing different bindings for deeper processing needs on pre-compiled level. First use case results with DLR's advanced concept for a suborbital, hypersonic, winged passenger transport vehicle called SpaceLiner show a real-time performance of an update rate of 50 Hz with 10 involved, distributed sub system modules. The use case implementation represents space vehicle specifics by extensions to the Space Reference Federation Object Model, a further domain specific standardization on federation object model level. Established a-priori interoperability will allow the independent development of the federation’s federates with a realistic inevitability that these parts of the distributed simulation will be able to smoothly interoperate. A position to future space / air traffic integration simulations is given and discussed. The paper concludes with an outlook on fusing possibilities with the air traffic management domain specific federation object model standard for future space / air traffic integration simulations.

elib-URL des Eintrags:https://elib.dlr.de/209413/
Dokumentart:Konferenzbeitrag (Vortrag)
Titel:The Space Liner Federation - Distributed Space Vehicle Simulation Based on Loose Coupling
Autoren:
AutorenInstitution oder E-Mail-AdresseAutoren-ORCID-iDORCID Put Code
Morlang, FrankFrank.Morlang (at) dlr.dehttps://orcid.org/0000-0003-3636-5215NICHT SPEZIFIZIERT
Strassburger, Steffensteffen.strassburger (at) tu-ilmenau.dehttps://orcid.org/0000-0003-0140-259X172523521
Datum:2024
Erschienen in:2024 IEEE Aerospace Conference, AERO 2024
Referierte Publikation:Ja
Open Access:Nein
Gold Open Access:Nein
In SCOPUS:Ja
In ISI Web of Science:Nein
DOI:10.1109/AERO58975.2024.10521195
ISSN:1095-323X
ISBN:979-835030462-6
Status:veröffentlicht
Stichwörter:HLA, distributed simulation
Veranstaltungstitel:2024 IEEE Aerospace Conference
Veranstaltungsort:Big Sky, MT, USA
Veranstaltungsart:internationale Konferenz
Veranstaltungsbeginn:2 März 2024
Veranstaltungsende:9 März 2024
Veranstalter :IEEE
HGF - Forschungsbereich:Luftfahrt, Raumfahrt und Verkehr
HGF - Programm:Luftfahrt
HGF - Programmthema:Luftverkehr und Auswirkungen
DLR - Schwerpunkt:Luftfahrt
DLR - Forschungsgebiet:L AI - Luftverkehr und Auswirkungen
DLR - Teilgebiet (Projekt, Vorhaben):L - Integrierte Flugführung
Standort: Braunschweig
Institute & Einrichtungen:Institut für Flugführung > ATM-Simulation
Hinterlegt von: Morlang, Frank
Hinterlegt am:26 Nov 2024 13:46
Letzte Änderung:26 Nov 2024 13:46

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