Aircraft Attitude Estimation- Euler angles / Quaternions
This MATLAB Simulink project computes Euler angles and quaternions from rate gyro data using Euler and Poisson kinematic equations.
https://github.com/Prajwal7r/Arcraft-AttitudeEstimation-Simulink
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Cite As
Prajwal N (2026). Aircraft Attitude Estimation- Euler angles / Quaternions (https://github.com/Prajwal7r/Arcraft-AttitudeEstimation-Simulink), GitHub. Retrieved .
General Information
- Version 1.0.0 (290 KB)
-
View License on GitHub
MATLAB Release Compatibility
- Compatible with any release
Platform Compatibility
- Windows
- macOS
- Linux
Versions that use the GitHub default branch cannot be downloaded
| Version | Published | Release Notes | Action |
|---|---|---|---|
| 1.0.0 |
To view or report issues in this GitHub add-on, visit the GitHub Repository.
To view or report issues in this GitHub add-on, visit the GitHub Repository.
