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@ -58,10 +58,12 @@ class Guidance {
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// @note: compares target Quaternion and reference quaternion, also actual satellite rate and
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// desired
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void comparePtg(double targetQuat[4], acsctrl::MekfData *mekfData, double quatRef[4], double refSatRate[3],
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double quatErrorComplete[4], double quatError[3], double deltaRate[3]);
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void comparePtg(double targetQuat[4], acsctrl::MekfData *mekfData, double quatRef[4],
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double refSatRate[3], double quatErrorComplete[4], double quatError[3],
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double deltaRate[3]);
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void refRotationRate(int8_t timeElapsedMax, timeval now, double quatInertialTarget[4], double *refSatRate);
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void refRotationRate(int8_t timeElapsedMax, timeval now, double quatInertialTarget[4],
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double *refSatRate);
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// @note: will give back the pseudoinverse matrix for the reaction wheel depending on the valid
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// reation wheel maybe can be done in "commanding.h"
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