Print Email Facebook Twitter An Anti-windup Fault Tolerant Control Scheme with Guaranteed Transient Performance for Tailless Flying Wing Aircraft Title An Anti-windup Fault Tolerant Control Scheme with Guaranteed Transient Performance for Tailless Flying Wing Aircraft Author Shuang, Weifang (Nanjing University of Aeronautics and Astronautics) Zhang, S. (Nanjing University of Aeronautics and Astronautics) Wu, Xue (Nanjing University of Aeronautics and Astronautics) van Kampen, E. (TU Delft Control & Simulation) Chu, Q. P. (TU Delft Control & Simulation) Date 2017 Abstract To reference this document use: http://resolver.tudelft.nl/uuid:e693923f-4907-445b-a6f9-5085383bdc0d DOI https://doi.org/10.2514/6.2017-1253 Publisher American Institute of Aeronautics and Astronautics Inc. (AIAA) Embargo date 2018-01-06 ISBN 978-1-62410-450-3 Source AIAA Guidance, Navigation, and Control Conference, 2017: January 9-13, Grapevine, TX Event AIAA Guidance, Navigation, and Control Conference, 2017, 2017-01-09 → 2017-01-13, Grapevine, United States Part of collection Institutional Repository Document type conference paper Rights © 2017 Weifang Shuang, S. Zhang, Xue Wu, E. van Kampen, Q. P. Chu Files PDF An_Anti_windup_Fault_Tole ... rcraft.pdf 556.4 KB Close viewer /islandora/object/uuid:e693923f-4907-445b-a6f9-5085383bdc0d/datastream/OBJ/view