all used guidance parts and their calls in AcsCrtl should work now
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@ -32,10 +32,6 @@ class Guidance {
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void targetQuatPtgNadirThreeAxes(timeval now, double posSatE[3], double velSatE[3],
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double targetQuat[4], double refSatRate[3]);
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// Function to get the target quaternion and refence rotation rate from parameters for inertial
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// pointing
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void targetQuatPtgInertial(double targetQuat[4], double targetSatRotRate[3]);
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// @note: Calculates the error quaternion between the current orientation and the target
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// quaternion, considering a reference quaternion. Additionally the difference between the actual
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// and a desired satellite rotational rate is calculated, again considering a reference rotational
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