What is it about?

A nonlinear dynamic model describing aircraft motion without a requirement for most stability derivatives or inertia information is introduced.

Featured Image

Read the Original

This page is a summary of: Minimum Parameter Approximation of Nonlinear Aircraft Dynamics, Journal of Guidance Control and Dynamics, August 2025, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.g008046.
You can read the full text:

Read

Contributors

Be the first to contribute to this page