dutch_roll
This MATLAB App is developed to simulate the Dutch Roll dynamic instability of an aircraft.
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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://in.mathworks.com/matlabcentral/fileexchange/180912-dutch_roll), MATLAB Central File Exchange. Retrieved .
Acknowledgements
Inspired by: Aircraft Control using Nonlinear Dynamic Inversion, Aircraft simulation
General Information
- Version 1.0.0 (25.4 KB)
MATLAB Release Compatibility
- Compatible with any release
Platform Compatibility
- Windows
- macOS
- Linux
| Version | Published | Release Notes | Action |
|---|---|---|---|
| 1.0.0 |
