diff --git a/mission/controller/acs/Guidance.cpp b/mission/controller/acs/Guidance.cpp
index 35a2f025..4368e014 100644
--- a/mission/controller/acs/Guidance.cpp
+++ b/mission/controller/acs/Guidance.cpp
@@ -539,18 +539,23 @@ ReturnValue_t Guidance::getDistributionMatrixRw(ACS::SensorValues *sensorValues,
   }
 }
 
-void Guidance::getTargetParamsSafe(double sunTargetSafe[3], double satRateSafe[3]) {
+void Guidance::getTargetParamsSafe(double sunTargetSafe[3], double satRateSafe[3],
+                                   double inertiaEive[3][3]) {
   std::error_code e;
   if (not std::filesystem::exists(SD_0_SKEWED_PTG_FILE, e) or
       not std::filesystem::exists(SD_1_SKEWED_PTG_FILE, e)) {
     std::memcpy(sunTargetSafe, acsParameters->safeModeControllerParameters.sunTargetDir,
-                3 * sizeof(double));
+                sizeof(&sunTargetSafe));
+    std::memcpy(inertiaEive, acsParameters->inertiaEIVE.inertiaMatrixDeployed,
+                sizeof(&inertiaEive));
   } else {
     std::memcpy(sunTargetSafe, acsParameters->safeModeControllerParameters.sunTargetDirLeop,
-                3 * sizeof(double));
+                sizeof(&sunTargetSafe));
+    std::memcpy(inertiaEive, acsParameters->inertiaEIVE.inertiaMatrixUndeployed,
+                sizeof(&inertiaEive));
   }
   std::memcpy(satRateSafe, acsParameters->safeModeControllerParameters.satRateRef,
-              3 * sizeof(double));
+              sizeof(&satRateSafe));
 }
 
 ReturnValue_t Guidance::solarArrayDeploymentComplete() {
diff --git a/mission/controller/acs/Guidance.h b/mission/controller/acs/Guidance.h
index f3369092..08183534 100644
--- a/mission/controller/acs/Guidance.h
+++ b/mission/controller/acs/Guidance.h
@@ -12,7 +12,7 @@ class Guidance {
   Guidance(AcsParameters *acsParameters_);
   virtual ~Guidance();
 
-  void getTargetParamsSafe(double sunTargetSafe[3], double satRateRef[3]);
+  void getTargetParamsSafe(double sunTargetSafe[3], double satRateRef[3], double inertiaEive[3][3]);
   ReturnValue_t solarArrayDeploymentComplete();
 
   // Function to get the target quaternion and refence rotation rate from gps position and