A toolbox for the main functions used in spacecraft attitude determination and control.
A- DCM to Quaternion
B- Quaternion to DCM
C- Euler to DCM
D- DCM to Euler
E- Euler to Quaternion
F- Quaternion to Euler
A- Biased Triad
B- Balanced Triad
C- Q-method
D- QUEST method
A- Sun Sensor (2D)
A- Non-Linear Equations of Motion
B- Linear Equations of Motion
Make sure all the files and folders are in your matlab path, and run "main.m" file.