Spacecraft Attitude Determination Using Global Positioning Satellite Signals



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Figure 3: Local orbital coordinate frame


For this coordinate frame, x is defined as the direction of satellite motion, y the orbit normal, and z completes a right-handed coordinate frame.

To rotate the position vectors into the local orbital frame, the vectors will first be rotated into the IJK coordinate frame using the following transformation matrix:



(8)

For which is the right ascension of the ascending node, is the argument of perigee, and is the inclination (Sellers). The vector is then rotated into the local orbital coordinate frame using the following transformation matrix:

(9)

For which



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