Final Version of the ACS Controller #367
@ -409,10 +409,6 @@ void Guidance::sunQuatPtg(ACS::SensorValues *sensorValues, acsctrl::MekfData *me
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double zAxis[3] = {0, 0, 0};
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VectorOperations<double>::normalize(sunDirB, zAxis, 3);
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// Position of satellite in ECEF
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double posSatE[3] = {0, 0, 0};
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std::memcpy(gpsDataProcessed->gpsPosition.value, posSatE, 3 * sizeof(double));
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// Assign helper vector (north pole inertial)
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double helperVec[3] = {0, 0, 1};
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