Attitude Calculation

Attitude calculation is the process of determining the orientation of a spacecraft or satellite with respect to a reference frame. This involves measuring the spacecraft's angular velocity, acceleration, and magnetic field, and using this information to calculate its attitude. Attitude calculation is critical for the proper functioning of a spacecraft, as it enables the accurate pointing of instruments and antennas, and the stabilization of the spacecraft's orientation. Attitude calculation is also important for navigation and control, as it allows the spacecraft to maintain a desired trajectory and avoid collisions with other objects in space.

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Attitude Calculation

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