The correct quadrants for <t> and ip are obtained from the relative signs of the elements of A in Eqs. (E-14a) and (E-I4c), respectively.

Kinematic Equations of Motion. For convenience, the kinematic equations of motion (Section 16.1) for the 12 possible Euler angle representations are given in Table E-2. The kinematic equations of motion for other representations of the attitude matrix can be found in Section 16.1.

Table E-2. Kinematic Equations of Motion For the 12 Possible Euler Angle Representations (I = jc axis, 2= y axis, 3=* axis; u„u2< uj components of the angular velocity along the body x,y, z axes.)
0 0

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