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Rodríguez Lucas, F. and Sanjurjo Rivo, Manuel and Pélaez Álvarez, Jesús (2015). Novel dynamical model for an object-oriented space tether simulator. In: "25th International Symposium on Space Flight Dynamics ISSFD", 19-23 oct 20015, Munich. pp. 1-19.
Title: | Novel dynamical model for an object-oriented space tether simulator |
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Author/s: |
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Item Type: | Presentation at Congress or Conference (Article) |
Event Title: | 25th International Symposium on Space Flight Dynamics ISSFD |
Event Dates: | 19-23 oct 20015 |
Event Location: | Munich |
Title of Book: | Proceedings of 25th International Symposium on Space Flight Dynamics ISSFD |
Título de Revista/Publicación: | Proceedings of 25th International Symposium on Space Flight Dynamics ISSFD |
Date: | October 2015 |
Subjects: | |
Freetext Keywords: | Simulation; tether; electrodynamic; dynamical model; multi-tethered systems |
Faculty: | E.T.S. de Ingeniería Aeronáutica y del Espacio (UPM) |
Department: | Física Aplicada a las Ingenierías Aeronáutica y Naval |
Creative Commons Licenses: | Recognition - No derivative works - Non commercial |
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This paper presents a novel dynamical model for space tether dynamics simulation. The proposed model discretises the cable in a number of elastic rods, which in turn are modeled as a set of equivalent masses. The orbital propagation is performed using a classical Cowell?s method and also a special perturbation method. The implementation is done within the framework of EcosimPro, a multidisciplinary simulation tool. A validation of the model is carried out, as well as a case of application to the de-orbiting of a satellite using an electrodynamic tether.
Item ID: | 52054 |
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DC Identifier: | https://oa.upm.es/52054/ |
OAI Identifier: | oai:oa.upm.es:52054 |
Official URL: | http://issfd.org/2015/index.php/final-program.html |
Deposited by: | Memoria Investigacion |
Deposited on: | 11 Feb 2019 11:16 |
Last Modified: | 11 Feb 2019 11:16 |