Quaternion Attitude Representation for Small Satellite

Quaternion Attitude Representation for Small Satellite Transformed from Euler Angles

• The subject of the program is to characterize the attitude dynamics of the Low Earth Orbit Satellite in terms of quaternions. Euler angles and angular velocity vectors taken from the first program and quaternion are found and then quaternion rates are found with these values. There are 4 parameters in quaternions, one of which is scalar, others are vectoral.