Validation of Space Net Deployment Modeling Methods Using Parabolic Flight Experiment
2017; American Institute of Aeronautics and Astronautics; Volume: 40; Issue: 12 Linguagem: Inglês
10.2514/1.g002761
ISSN1533-3884
AutoresMinghe Shan, Jian Guo, E. Gill, Wojciech Gołębiowski,
Tópico(s)Distributed Control Multi-Agent Systems
ResumoNo AccessEngineering NoteValidation of Space Net Deployment Modeling Methods Using Parabolic Flight ExperimentMinghe Shan, Jian Guo, Eberhard Gill and Wojciech GołębiowskiMinghe ShanDelft University of Technology, Delft HS 2629, The Netherlands, Jian GuoDelft University of Technology, Delft HS 2629, The Netherlands, Eberhard GillDelft University of Technology, Delft HS 2629, The Netherlands and Wojciech GołębiowskiSKA Polska, 02-017 Warsaw, PolandPublished Online:1 Aug 2017https://doi.org/10.2514/1.G002761SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookTwitterLinked InRedditEmail About References [1] Shan M., Guo J. and Gill E., "Review and Comparison of Active Space Debris Capturing and Removal Methods," Progress in Aerospace Sciences, Vol. 80, Jan. 2016, pp. 18–32. doi:https://doi.org/10.1016/j.paerosci.2015.11.001 PAESD6 0376-0421 CrossrefGoogle Scholar[2] Reintsema D., Thaeter J., Rathke A., Naumann W., Rank P. and Sommer J., "DEOS—The German Robotics Approach to Secure and De-Orbit Malfunctioned Satellites from Low Earth Orbits," Proceedings of the i-SAIRAS, Japan Aerospace Exploration Agency (JAXA), Sapporo, Japan, 2010, pp. 244–251. 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Published by the American Institute of Aeronautics and Astronautics, Inc., with permission. All requests for copying and permission to reprint should be submitted to CCC at www.copyright.com; employ the ISSN 0731-5090 (print) or 1533-3884 (online) to initiate your request. See also AIAA Rights and Permissions www.aiaa.org/randp. TopicsComputational Fluid DynamicsFinite Element MethodFluid DynamicsGyroscopesMechanical and Structural VibrationsMultibody SystemNumerical AnalysisNumerical InterpolationStructural AnalysisStructural Design and DevelopmentStructural EngineeringStructural Kinematics and DynamicsStructures, Design and TestVibration Measuring Instruments KeywordsAeroplaneCoriolis EffectSpace DebrisESAFinite Element MethodMicrogravityEarth Centered InertialLagrange MultipliersElastic ModulusLinear InterpolationAcknowledgmentsThe authors wish to acknowledge the help given by Kjetil Wormnes, who is a Mechatronics Engineer from the ESA, and the experimental data set shared by the ESA. In addition, the first author, Minghe Shan, acknowledges the financial support of the Chinese Scholarship Council for Ph.D. Scholarship.PDF Received17 January 2017Accepted19 May 2017Published online1 August 2017
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