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Path: Common/Transform
-------------------------------------------------------------------------- Converts 3-2-1 Euler angle rates into angular velocity. If only one input is given, the output is the transformation matrix. -------------------------------------------------------------------------- Form: w = EulDot2Rates( e, wEul, n ) -------------------------------------------------------------------------- ------ Inputs ------ e (3) Euler angles wEul (3) Angular rates n (1) Orbit rate (for rotating frames only, optional) ------- Outputs ------- w (3) Euler angle rates -------------------------------------------------------------------------- Reference: Hughes, Spacecraft Attitude Dynamics (1986), Eq. 25 p. 27 --------------------------------------------------------------------------
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