Aircraft Attitude Estimation- Euler angles / Quaternions

Version 1.0.0 (290 KB) by Prajwal N
This MATLAB Simulink project computes Euler angles and quaternions from rate gyro data using Euler and Poisson kinematic equations.
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Updated 3 May 2025
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Cite As

Prajwal N (2026). Aircraft Attitude Estimation- Euler angles / Quaternions (https://github.com/Prajwal7r/Arcraft-AttitudeEstimation-Simulink), GitHub. Retrieved .

MATLAB Release Compatibility
Created with R2022b
Compatible with any release
Platform Compatibility
Windows macOS Linux
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Version Published Release Notes
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.