diff --git a/mission/controller/AcsController.cpp b/mission/controller/AcsController.cpp
index 557a6105..8b3eee64 100644
--- a/mission/controller/AcsController.cpp
+++ b/mission/controller/AcsController.cpp
@@ -368,9 +368,11 @@ void AcsController::performPointingCtrl() {
   // Variables required for setting actuators
   double torquePtgRws[4] = {0, 0, 0, 0}, rwTrqNs[4] = {0, 0, 0, 0}, torqueRws[4] = {0, 0, 0, 0},
          mgtDpDes[3] = {0, 0, 0};
+
   switch (mode) {
     case acs::PTG_IDLE:
-      guidance.targetQuatPtgSun(susDataProcessed.sunIjkModel.value, targetQuat, targetSatRotRate);
+      guidance.targetQuatPtgSun(now, susDataProcessed.sunIjkModel.value, targetQuat,
+                                targetSatRotRate);
       guidance.comparePtg(mekfData.quatMekf.value, mekfData.satRotRateMekf.value, targetQuat,
                           targetSatRotRate, errorQuat, errorSatRotRate, errorAngle);
       ptgCtrl.ptgLaw(&acsParameters.idleModeControllerParameters, errorQuat, errorSatRotRate,
@@ -460,7 +462,7 @@ void AcsController::performPointingCtrl() {
 
     case acs::PTG_INERTIAL:
       std::memcpy(targetQuat, acsParameters.inertialModeControllerParameters.tgtQuat,
-                  4 * sizeof(double));
+                  sizeof(targetQuat));
       guidance.comparePtg(mekfData.quatMekf.value, mekfData.satRotRateMekf.value, targetQuat,
                           targetSatRotRate, acsParameters.inertialModeControllerParameters.quatRef,
                           acsParameters.inertialModeControllerParameters.refRotRate, errorQuat,