diff --git a/matlab/unstable_examples/+imuSimulator/testCoriolis.m b/matlab/unstable_examples/+imuSimulator/coriolisExample.m
similarity index 70%
rename from matlab/unstable_examples/+imuSimulator/testCoriolis.m
rename to matlab/unstable_examples/+imuSimulator/coriolisExample.m
index d79589ca5..9599c2508 100644
--- a/matlab/unstable_examples/+imuSimulator/testCoriolis.m
+++ b/matlab/unstable_examples/+imuSimulator/coriolisExample.m
@@ -1,27 +1,38 @@
+%% coriolisExample.m
+% Author(s): David Jensen (david.jensen@gtri.gatech.edu)
+% This script demonstrates the relationship between object motion in inertial and rotating reference frames.
+% For this example, we consider a fixed (inertial) reference frame located at the center of the earth and initially 
+% coincident with the rotating ECEF reference frame (X towards 0 longitude, Y towards 90 longitude, Z towards 90 latitude),
+% which rotates with the earth.
+% A body is moving in the positive Z-direction and positive Y-direction with respect to the fixed reference frame.
+% Its position is plotted in both the fixed and rotating reference frames to simulate how an observer in each frame would
+% experience the body's motion.
+
 clc
 clear all
 close all
 
 import gtsam.*;
 
+%% General configuration
 deltaT = 0.1;
 timeElapsed = 10;
 times = 0:deltaT:timeElapsed;
 
 %omega = [0;0;7.292115e-5]; % Earth Rotation
 omega = [0;0;5*pi/10];
-velocity = [0;0;0];         % initially not moving
-accelFixed = [0;0.1;0.1];     % accelerate in the positive z-direction
+velocity = [0;0;0];                 % initially not moving
+accelFixed = [0;0.1;0.1];           % accelerate in the positive z-direction
 initialPosition = [0; 1.05; 0];     % start along the positive x-axis
 
-% Initial state
+%% Initial state of the body in the fixed in rotating frames should be the same
 currentPoseFixedGT = Pose3(Rot3, Point3(initialPosition));
 currentVelocityFixedGT = velocity;
 
 currentPoseRotatingGT = currentPoseFixedGT;
 currentPoseRotatingFrame = Pose3;
 
-% Positions
+%% Initialize storage variables
 positionsFixedGT = zeros(3, length(times)+1);
 positionsRotatingGT = zeros(3, length(times)+1);
 
@@ -35,10 +46,13 @@ poses(1).R = currentPoseRotatingFrame.rotation.matrix;
 
 h = figure(1);
 
+%% Main loop: iterate through 
 i = 2;
 for t = times
     %% Create ground truth trajectory
-    % Update the pose and velocity
+    % Update the position and velocity
+    % x_t = x_0 + v_0*dt + 1/2*a_0*dt^2
+    % v_t = v_0 + a_0*dt
     currentPositionFixedGT = Point3(currentPoseFixedGT.translation.vector ...
         + currentVelocityFixedGT * deltaT + 0.5 * accelFixed * deltaT * deltaT);
     currentVelocityFixedGT = currentVelocityFixedGT + accelFixed * deltaT;
@@ -55,7 +69,7 @@ for t = times
     poses(i).p = currentPoseRotatingFrame.translation.vector;
     poses(i).R = currentPoseRotatingFrame.rotation.matrix;
     
-    % incremental graphing
+    % incremental plotting for animation
     figure(h)
     plot_trajectory(poses(i),1, '-k', 'Rotating Frame',0.1,0.75,1)
     hold on;
@@ -76,10 +90,11 @@ for t = times
     i = i + 1;
 end
 
-
+%% Final plotting
 figure
-sphere
+sphere  % sphere for reference
 hold on;
+% trajectories in Fixed and Rotating frames
 plot3(positionsFixedGT(1,:), positionsFixedGT(2,:), positionsFixedGT(3,:));
 plot3(positionsRotatingGT(1,:), positionsRotatingGT(2,:), positionsRotatingGT(3,:), '-r');