diff --git a/include/outVector.h b/include/outVector.h
index a0d6247..1e08f4b 100644
--- a/include/outVector.h
+++ b/include/outVector.h
@@ -33,9 +33,6 @@ struct outVector {
 
   std::vector<double> LQRx = std::vector<double>(length, 0.0);
   std::vector<double> LQRy = std::vector<double>(length, 0.0);
-
-  std::vector<double> thrust = std::vector<double>(length, 0.0);
-  std::vector<double> d_yError = std::vector<double>(length, 0.0);
 };
 
 #endif
\ No newline at end of file
diff --git a/include/sim.h b/include/sim.h
index ab883df..0f10021 100644
--- a/include/sim.h
+++ b/include/sim.h
@@ -376,8 +376,6 @@ void state2vec(Vehicle &State, Vehicle &PrevState, outVector &stateVector,
 
   stateVector.LQRx[t] = State.LQRx;
   stateVector.LQRy[t] = State.LQRy;
-  stateVector.thrust[t] = State.thrust;
-  stateVector.d_yError[t] = State.d_yError;
 
   // Set "prev" values for next timestep
   PrevState = State;
@@ -434,9 +432,7 @@ void write2CSV(outVector &stateVector, Vehicle &State) {
     outfile << stateVector.thrustFiring[t] << ", ";
 
     outfile << stateVector.LQRx[t] << ", ";
-    outfile << stateVector.LQRy[t] << ", ";
-    outfile << stateVector.thrust[t] << ", ";
-    outfile << stateVector.d_yError[t] << std::endl;
+    outfile << stateVector.LQRy[t] << std::endl;
   }
 
   outfile.close();
diff --git a/matlabHelpers/Untitled.asv b/matlabHelpers/Untitled.asv
deleted file mode 100644
index 268daf9..0000000
--- a/matlabHelpers/Untitled.asv
+++ /dev/null
@@ -1,13 +0,0 @@
-clear all; close all; clc;
-
-syms I11 I22 I33 I11dot I22dot I33dot
-
-I =  [I11 0 0; 0 I22 0; 0 0 I33];
-Idot =  [I11dot 0 0; 0 I22dot 0; 0 0 I33dot];
-
-syms yaw pitch roll yawdot pitchdot rolldot yawddot pitchddot rollddot
-
-w = 
-
-I * 
-
diff --git a/matlabHelpers/Untitled.m b/matlabHelpers/Untitled.m
deleted file mode 100644
index 8842322..0000000
--- a/matlabHelpers/Untitled.m
+++ /dev/null
@@ -1,24 +0,0 @@
-clear all; close all; clc;
-
-syms I11 I22 I33 I11dot I22dot I33dot
-
-I =  [I11 0 0; 0 I22 0; 0 0 I33];
-Idot =  [I11dot 0 0; 0 I22dot 0; 0 0 I33dot];
-
-syms yaw pitch roll yawdot pitchdot rolldot yawddot pitchddot rollddot
-
-w = [yawdot; pitchdot; rolldot];
-
-Iw = I * w;
-Idw = Idot * w;
-
-C = cross(w, Iw);
-
-syms momentX momentY momentZ
-
-M = [momentX; momentY; momentZ];
-A = M - Idw - C;
-B = [A(1) A(2) A(3)];
-
-X = B*inv(I);
-E = [X(1); X(2); X(3)]
\ No newline at end of file