GitHub Pages Setup

- Update README with link to project website
- Add proposal pdf to docs folder
- Add whitespace to PlantModel.m
- Add home.md as homepage of website

README.md

@@ -1,3 +1,9 @@
 # Quadcopter Control
 
-ME/EECS 561 W20 Quadcopter control source code repository.
+UMICH EECS / MECHENG 561: Design of Digital Control Systems WN 2020
+
+Full State Feedback and Control of a Quadcopter Drone
+
+## Documentation
+
+Please see the project [website](https://me-561-w20-quadcopter-project.github.io/Quadcopter-Control/home) for documentation.

docs/home.md

@@ -0,0 +1,25 @@
+# Full State Feedback and Control of a Quadcopter Drone <!-- omit in toc -->
+
+## Table of Contents <!-- omit in toc -->
+- [Contributors](#contributors)
+- [Documents](#documents)
+
+## Contributors
+
+### Project Team <!-- omit in toc -->
+
+- Sravan Balaji ([balajsra@umich.edu](mailto:balajsra@umich.edu))
+- Aditya Iyer ([adiyer@umich.edu](mailto:adiyer@umich.edu))
+- Lakshmanan Periakaruppan ([lperiaka@umich.edu](mailto:lperiaka@umich.edu))
+- Naman Shah ([namanvs@umich.edu](mailto:namanvs@umich.edu))
+- Sumedh Vaishampayan ([sumi@umich.edu](mailto:sumi@umich.edu))
+
+### EECS / MECHENG 561 W20 Course Staff <!-- omit in toc -->
+
+- Ram Vasudevan ([ramv@umich.edu](mailto:ramv@umich.edu))
+- Sid Dey ([siddey@umich.edu](mailto:siddey@umich.edu))
+
+## Documents
+
+1. [Project Proposal](1.%20ME%20561%20Project%20Proposal.pdf)
+2. [Final Report (Overleaf)](https://www.overleaf.com/read/kyjvdsxkfnmg)

src/PlantModel.m

@@ -1,19 +1,19 @@
-%Parameters source: https://sal.aalto.fi/publications/pdf-files/eluu11_public.pdf
+% Parameters source: https://sal.aalto.fi/publications/pdf-files/eluu11_public.pdf
 g=9.81;
 m = .468;
 Ix = 4.856*10^-3;
 Iy = 4.856*10^-3;
 Iz = 8.801*10^-3;
 
-%State Space Source: https://arxiv.org/ftp/arxiv/papers/1908/1908.07401.pdf
+% State Space Source: https://arxiv.org/ftp/arxiv/papers/1908/1908.07401.pdf
-%X' = Ax+Bu
+% X' = Ax+Bu
-%y = Cx+Du
+% y = Cx+Du
 
-%Inputs:
+% Inputs:
-%U1: Total Upward Force on the quad rotor along z-axis
+% U1: Total Upward Force on the quad rotor along z-axis
-%U2: Pitch Torque (about x-axis)
+% U2: Pitch Torque (about x-axis)
-%U3: Roll Torque (about y-axis)
+% U3: Roll Torque (about y-axis)
-%U4: Yaw Torque (about z-axis)
+% U4: Yaw Torque (about z-axis)
 A = [0  0  0  1  0  0  0  0  0  0  0  0;...
      0  0  0  0  1  0  0  0  0  0  0  0;...
      0  0  0  0  0  1  0  0  0  0  0  0;...
@@ -27,7 +27,7 @@ A = [0  0  0  1  0  0  0  0  0  0  0  0;...
      0  0  0  0  0  0  0  0  0  0  0  0;...
      0  0  0  0  0  0  0  0  0  0  0  0];
 
-%Note: In paper, 1/m is in wrong spot
+% Note: In paper, 1/m is in wrong spot
 B = [0 0 0 0;...
      0 0 0 0;...
      0 0 0 0;...
@@ -40,13 +40,12 @@ B = [0 0 0 0;...
      0 1/Ix 0 0;...
      0 0 1/Iy 0;...
      0 0 0 1/Iz];
+
 C = [1 0 0 0 0 0 0 0 0 0 0 0;...
      0 1 0 0 0 0 0 0 0 0 0 0;...
      0 0 1 0 0 0 0 0 0 0 0 0;...
      0 0 0 0 0 0 1 0 0 0 0 0;...
      0 0 0 0 0 0 0 1 0 0 0 0;...
-     0 0 0 0 0 0 0 0 1 0 0 0]
+     0 0 0 0 0 0 0 0 1 0 0 0];
-D = zeros(6,4)
-     
-
 
+D = zeros(6,4);