Onboard Trajectory Generation for Entry Vehicles via Adaptive Multivariate Pseudospectral Interpolation
2016; American Institute of Aeronautics and Astronautics; Volume: 40; Issue: 2 Linguagem: Inglês
10.2514/1.g001817
ISSN1533-3884
AutoresMarco Sagliano, Erwin Mooij, Stephan Theil,
Tópico(s)Space Satellite Systems and Control
ResumoNo AccessComputational Guidance and ControlOnboard Trajectory Generation for Entry Vehicles via Adaptive Multivariate Pseudospectral InterpolationMarco Sagliano, Erwin Mooij and Stephan TheilMarco SaglianoDLR, German Aerospace Center, 28359 Bremen, Germany*Research Engineer, Guidance, Navigation and Control Department, Robert Hooke Straße 7. Member AIAA.Search for more papers by this author, Erwin MooijDelft University of Technology, 2629 HS Delft, The Netherlands†Assistant Professor, Astrodynamics and Space Missions Department, Faculty of Aerospace Engineering, Kluyverweg 1. Associate Fellow AIAA.Search for more papers by this author and Stephan TheilDLR, German Aerospace Center, 28359 Bremen, Germany‡Head, Guidance, Navigation and Control Department, Robert Hooke Straße 7.Search for more papers by this authorPublished Online:16 Sep 2016https://doi.org/10.2514/1.G001817SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookTwitterLinked InRedditEmail About References [1] Harpold J. C. and Graves C. A., “Shuttle Entry Guidance,” Journal of the Astronautical Sciences, Vol. 27, No. 3, 1979, pp. 239–268. JALSA6 0021-9142 Google Scholar[2] Lu P., “Entry Guidance: A Unified Method,” Journal of Guidance, Control, and Dynamics, Vol. 37, No. 3, 2014, pp. 713–728. doi:https://doi.org/10.2514/1.62605 JGCODS 0731-5090 LinkGoogle Scholar[3] Mease K. D., Chen D. 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