dutch_roll
Version 1.0.0 (25.4 KB) by
Vignesh
This MATLAB App is developed to simulate the Dutch Roll dynamic instability of an aircraft.
This MATLAB App provides a user-friendly interface to study the Dutch Roll instability in aircraft, a type of lateral-directional oscillation that occurs due to the coupling between yaw and roll motions. The app enables users to input initial conditions—such as the initial sideslip angle (β in degrees)—and aircraft-specific parameters that influence stability.
Cite As
Vignesh (2026). dutch_roll (https://se.mathworks.com/matlabcentral/fileexchange/180912-dutch_roll), MATLAB Central File Exchange. Retrieved .
MATLAB Release Compatibility
Created with
R2024b
Compatible with any release
Platform Compatibility
Windows macOS LinuxTags
Acknowledgements
Inspired by: Aircraft Control using Nonlinear Dynamic Inversion, Aircraft simulation
Discover Live Editor
Create scripts with code, output, and formatted text in a single executable document.
| Version | Published | Release Notes | |
|---|---|---|---|
| 1.0.0 |
