mirror of
https://github.com/ME-561-W20-Quadcopter-Project/Quadcopter-Control.git
synced 2025-09-02 05:33:14 +00:00
IMU Sensor Model
- Remove gitignore from src folder - Add whitespace and parameterize desired position to Plant Model - Add IMU-like sensor model to plant model with sensor
This commit is contained in:
4
src/.gitignore
vendored
4
src/.gitignore
vendored
@@ -1,4 +0,0 @@
|
||||
*.slxc
|
||||
*.slx.autosave
|
||||
*.asv
|
||||
slprj
|
@@ -1,19 +1,24 @@
|
||||
%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;
|
||||
% Clear Workspace
|
||||
clear all;
|
||||
close all;
|
||||
clc;
|
||||
|
||||
%State Space Source: https://arxiv.org/ftp/arxiv/papers/1908/1908.07401.pdf
|
||||
%X' = Ax+Bu
|
||||
%y = Cx+Du
|
||||
% Parameters source: https://sal.aalto.fi/publications/pdf-files/eluu11_public.pdf
|
||||
g = 9.81;
|
||||
m = 0.468;
|
||||
Ix = 4.856E-3;
|
||||
Iy = 4.856E-3;
|
||||
Iz = 8.801E-3;
|
||||
|
||||
%Inputs:
|
||||
%U1: Total Upward Force on the quad rotor along z-axis
|
||||
%U2: Pitch Torque (about x-axis)
|
||||
%U3: Roll Torque (about y-axis)
|
||||
%U4: Yaw Torque (about z-axis)
|
||||
% State Space Source: https://arxiv.org/ftp/arxiv/papers/1908/1908.07401.pdf
|
||||
% X' = Ax+Bu
|
||||
% y = Cx+Du
|
||||
|
||||
% Inputs:
|
||||
% U1: Total Upward Force on the quad rotor along z-axis
|
||||
% U2: Pitch Torque (about x-axis)
|
||||
% U3: Roll Torque (about y-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 +32,7 @@ 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;...
|
||||
@@ -45,8 +50,8 @@ C = [1 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 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]
|
||||
D = zeros(6,4)
|
||||
0 0 0 0 0 0 0 0 1 0 0 0];
|
||||
D = zeros(6,4);
|
||||
sys = ss(A,B,C,D);
|
||||
sysd = c2d(sys, 1/100);
|
||||
|
||||
@@ -56,19 +61,24 @@ z0 = 0;
|
||||
xdot0 = 0;
|
||||
ydot0 = 0;
|
||||
zdot0 = 0;
|
||||
phi0 = 5*(pi/180)*0;
|
||||
theta0 = 5*(pi/180)*0;
|
||||
%phi0 = 5*(pi/180);
|
||||
phi0 = 0;
|
||||
%theta0 = 5*(pi/180);
|
||||
theta0 = 0;
|
||||
psi0 = 0;
|
||||
phidot0 = 0;
|
||||
thetadot0 = 0;
|
||||
psidot0 = 0;
|
||||
initialCondition = [x0, y0, z0, xdot0, ydot0, zdot0, phi0, theta0, psi0, phidot0, thetadot0, psidot0];
|
||||
|
||||
x_d = 1;
|
||||
y_d = 1;
|
||||
z_d = 1;
|
||||
|
||||
%%
|
||||
%Gains
|
||||
kpp = 0.4754;
|
||||
kdp = .1;
|
||||
kdp = 0.1;
|
||||
|
||||
kpt = 0.4754;
|
||||
kdt = 0.1;
|
||||
@@ -78,8 +88,3 @@ kdps = 0.0486;
|
||||
|
||||
kpz = 4.0670;
|
||||
kdz = 2.9031;
|
||||
|
||||
Q = zeros(12); Q(7:9, 7:9) = eye(3);
|
||||
R = 1;
|
||||
%K = lqr(A,B,Q,R);
|
||||
|
||||
|
Binary file not shown.
BIN
src/PlantModelWithSensorSim.slx
Normal file
BIN
src/PlantModelWithSensorSim.slx
Normal file
Binary file not shown.
Reference in New Issue
Block a user