applyed CppStyle Format

mission/controller/acs/AcsParameters.h

@@ -816,49 +816,48 @@ class AcsParameters : public HasParametersIF {
   } safeModeControllerParameters;
 
   struct PointingLawParameters {
+    double zeta = 0.3;
+    double om = 0.3;
+    double omMax = 1 * M_PI / 180;
+    double qiMin = 0.1;
+    double gainNullspace = 0.01;
 
-	double zeta = 0.3;
-	double om = 0.3;
-	double omMax = 1 * M_PI / 180;
-	double qiMin = 0.1;
-	double gainNullspace = 0.01;
-
-	double desatMomentumRef[3] = {0, 0, 0};
-	double deSatGainFactor = 1000;
-	uint8_t desatOn = true;
-	uint8_t enableAntiStiction = true;
+    double desatMomentumRef[3] = {0, 0, 0};
+    double deSatGainFactor = 1000;
+    uint8_t desatOn = true;
+    uint8_t enableAntiStiction = true;
 
   } pointingLawParameters;
 
   struct TargetModeControllerParameters : PointingLawParameters {
-	double refDirection[3] = {-1, 0, 0};  // Antenna
-	double refRotRate[3] = {0, 0, 0}; // Not used atm, do we want an option to
-	// give this as an input- currently en calculation is done
-	double quatRef[4] = {0, 0, 0, 1};
-	int8_t timeElapsedMax = 10; // rot rate calculations
+    double refDirection[3] = {-1, 0, 0};  // Antenna
+    double refRotRate[3] = {0, 0, 0};     // Not used atm, do we want an option to
+    // give this as an input- currently en calculation is done
+    double quatRef[4] = {0, 0, 0, 1};
+    int8_t timeElapsedMax = 10;  // rot rate calculations
 
-	// Default is Stuttgart GS
-	double latitudeTgt = 48.7495 * M_PI / 180.;   // [rad] Latitude
-	double longitudeTgt = 9.10384 * M_PI / 180.;  // [rad] Longitude
-	double altitudeTgt = 500; // [m]
+    // Default is Stuttgart GS
+    double latitudeTgt = 48.7495 * M_PI / 180.;   // [rad] Latitude
+    double longitudeTgt = 9.10384 * M_PI / 180.;  // [rad] Longitude
+    double altitudeTgt = 500;                     // [m]
 
-	// For one-axis control:
-	uint8_t avoidBlindStr = true;
-	double blindAvoidStart = 1.5;
-	double blindAvoidStop = 2.5;
-	double blindRotRate = 1 * M_PI / 180;
+    // For one-axis control:
+    uint8_t avoidBlindStr = true;
+    double blindAvoidStart = 1.5;
+    double blindAvoidStop = 2.5;
+    double blindRotRate = 1 * M_PI / 180;
   } targetModeControllerParameters;
 
   struct NadirModeControllerParameters : PointingLawParameters {
-	double refDirection[3] = {-1, 0, 0};  // Antenna
-	double quatRef[4] = {0, 0, 0, 1};
-    int8_t timeElapsedMax = 10; // rot rate calculations
+    double refDirection[3] = {-1, 0, 0};  // Antenna
+    double quatRef[4] = {0, 0, 0, 1};
+    int8_t timeElapsedMax = 10;  // rot rate calculations
   } nadirModeControllerParameters;
 
   struct InertialModeControllerParameters : PointingLawParameters {
-	double tgtQuat[4] = {0, 0, 0, 1};
-	double refRotRate[3] = {0, 0, 0};
-	double quatRef[4] = {0, 0, 0, 1};
+    double tgtQuat[4] = {0, 0, 0, 1};
+    double refRotRate[3] = {0, 0, 0};
+    double quatRef[4] = {0, 0, 0, 1};
   } inertialModeControllerParameters;
 
   struct StrParameters {