Final Version of the ACS Controller #367
@ -415,9 +415,9 @@ void Guidance::sunQuatPtg(ACS::SensorValues *sensorValues, acsctrl::MekfData *me
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// Assign helper vector (north pole inertial) accordingly
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double helperVec[3] = {0, 0, 0};
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if (posSatE[2] > 0) {
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double helperVec[2] = 1;
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helperVec[2] = 1;
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} else {
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double helperVec[2] = -1;
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helperVec[2] = -1;
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}
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//
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