Question: Your spacecraft in low Earth orbit has (3-2-1) Euler angles (30 deg, 48 deg, 10 deg) describ- ing its current attitude with respect to the
Your spacecraft in low Earth orbit has (3-2-1) Euler angles (30 deg, 48 deg, 10 deg) describ- ing its current attitude with respect to the Earth Centered Inertial (ECI) frame. You are interested in docking onto the space station, which has an attitude relative to the same ECI frame given by the Euler parameters (0,1,2,3) = (0.8047,0.3970,0.1000,0.4299). What is the attitude of your spacecraft relative to the space station?
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