What is it about?
This paper designs a nonlinear controller which could alleviate the gust load of a flexible aircraft.
Featured Image
Read the Original
This page is a summary of: Flexible Aircraft Gust Load Alleviation with Incremental Nonlinear Dynamic Inversion, Journal of Guidance Control and Dynamics, July 2019, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.g003980.
You can read the full text:
Contributors
The following have contributed to this page
