Singh, Sunayna und Mastrogiuseppe, Matteo (2024) Multibody modelling of tether and capture system for dynamic simulations of In-Air Capturing. Acta Astronautica, 218, Seiten 59-69. Elsevier. doi: 10.1016/j.actaastro.2024.02.008. ISSN 0094-5765.
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Offizielle URL: https://www.sciencedirect.com/science/article/pii/S0094576524000663?via%3Dihub
Kurzfassung
The launcher recovery method known as `In-Air Capturing' is an innovative approach where a winged rocket stage is captured mid-air by an aircraft and subsequently towed back to the launch site. To achieve this, a capturing device attached to a tether is released from the towing aircraft. This device autonomously connects the reusable launch vehicle to the aircraft, while the two vehicles are in proximity. The flexible dynamics of the tether have a strong influence on the maneuverability of the capturing device. Thus, it is critical to model the dynamics of the tether to get a realistic understanding and to evaluate feasibility of the concept. However, precise modelling and control of highly flexible systems with large deformations is both challenging and computationally intensive. For engineering applications which involve closed-loop simulations, finding a trade-off between accuracy and computational effort is crucial. In this paper, the tether is modelled as a discretized chain of rigid bodies connected by rotational springs at the joints. The tether along with the capture system is integrated in a simulation model and open loop tests are performed to analyze the system characteristics. The tether properties are studied to find a suited configuration for `In-Air Capturing'.
elib-URL des Eintrags: | https://elib.dlr.de/202886/ | ||||||||||||
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Dokumentart: | Zeitschriftenbeitrag | ||||||||||||
Titel: | Multibody modelling of tether and capture system for dynamic simulations of In-Air Capturing | ||||||||||||
Autoren: |
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Datum: | 2024 | ||||||||||||
Erschienen in: | Acta Astronautica | ||||||||||||
Referierte Publikation: | Ja | ||||||||||||
Open Access: | Ja | ||||||||||||
Gold Open Access: | Nein | ||||||||||||
In SCOPUS: | Ja | ||||||||||||
In ISI Web of Science: | Ja | ||||||||||||
Band: | 218 | ||||||||||||
DOI: | 10.1016/j.actaastro.2024.02.008 | ||||||||||||
Seitenbereich: | Seiten 59-69 | ||||||||||||
Verlag: | Elsevier | ||||||||||||
Name der Reihe: | ASCenSIon: Advancing Space Access Capabilities | ||||||||||||
ISSN: | 0094-5765 | ||||||||||||
Status: | veröffentlicht | ||||||||||||
Stichwörter: | Flexible tether dynamics, large deflection problem, closed-loop multibody systems, In-Air Capturing, reusable launch technology | ||||||||||||
HGF - Forschungsbereich: | Luftfahrt, Raumfahrt und Verkehr | ||||||||||||
HGF - Programm: | Raumfahrt | ||||||||||||
HGF - Programmthema: | Raumtransport | ||||||||||||
DLR - Schwerpunkt: | Raumfahrt | ||||||||||||
DLR - Forschungsgebiet: | R RP - Raumtransport | ||||||||||||
DLR - Teilgebiet (Projekt, Vorhaben): | R - Systemanalyse Raumtransport (SART) | ||||||||||||
Standort: | Bremen | ||||||||||||
Institute & Einrichtungen: | Institut für Raumfahrtsysteme > Systemanalyse Raumtransport | ||||||||||||
Hinterlegt von: | Singh, Sunayna | ||||||||||||
Hinterlegt am: | 04 Mär 2024 09:24 | ||||||||||||
Letzte Änderung: | 05 Apr 2024 11:45 |
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