Print Email Facebook Twitter Model Verification of a Satellite with Large Flexible Appendages for Control System Design Title Model Verification of a Satellite with Large Flexible Appendages for Control System Design Author Mooij, E. (TU Delft Astrodynamics & Space Missions) Gransden, D.I. (TU Delft Structural Integrity & Composites) Date 2018-01-01 Abstract To reference this document use: http://resolver.tudelft.nl/uuid:22e0d379-a6b3-49e2-9ce5-430a32e7913e DOI https://doi.org/10.2514/6.2018-0209 Publisher American Institute of Aeronautics and Astronautics Inc. (AIAA) Embargo date 2019-02-01 ISBN 978-1-5108-5701-8 Source AIAA Guidance, Navigation, and Control (210039) Event AIAA Guidance, Navigation, and Control Conference, 2018, 2018-01-08 → 2018-01-12, Kissimmee, United States Part of collection Institutional Repository Document type conference paper Rights © 2018 E. Mooij, D.I. Gransden Files PDF AIAA_2018_0209.pdf 1.3 MB Close viewer /islandora/object/uuid:22e0d379-a6b3-49e2-9ce5-430a32e7913e/datastream/OBJ/view