Correction: Design and Evaluation of Nonlinear Inversion Based Automated Landing Control for an Airliner in a High Crosswind Scenario (American Institute of Aeronautics and Astronautics Inc, AIAA)
Publication Date
1-1-2025
Document Type
Article
Publication Title
AIAA Science and Technology Forum and Exposition AIAA Scitech Forum 2025
DOI
10.2514/6.2025-0079.c1
Abstract
Change copyright listed in the first page to : Copyright © by Ho Joong Kim, Thomas Lombaerts, Gertjan Looye. Published by the American Institute of Aeronautics and Astronautics, Inc., with permission.
Department
Aerospace Engineering
Recommended Citation
Ho Joong Kim, Thomas Lombaerts, and Gertjan Looye. "Correction: Design and Evaluation of Nonlinear Inversion Based Automated Landing Control for an Airliner in a High Crosswind Scenario (American Institute of Aeronautics and Astronautics Inc, AIAA)" AIAA Science and Technology Forum and Exposition AIAA Scitech Forum 2025 (2025). https://doi.org/10.2514/6.2025-0079.c1
COinS
