Added PD controller

This commit is contained in:
Lakshu Periakaruppan
2020-04-11 15:11:34 -04:00
parent d463ccf0ac
commit 0de43c3cb8
3 changed files with 81 additions and 51 deletions

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*.slxc
*.slx.autosave
*.asv
slprj

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% 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; g=9.81;
m = .468; m = .468;
Ix = 4.856*10^-3; Ix = 4.856*10^-3;
Iy = 4.856*10^-3; Iy = 4.856*10^-3;
Iz = 8.801*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;... 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 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 0 0 0;...
0 0 0 0 0 0 0 -g 0 0 0 0;... 0 0 0 0 0 0 0 -g 0 0 0 0;...
0 0 0 0 0 0 g 0 0 0 0 0;... 0 0 0 0 0 0 g 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 0 0 0 0 0 0 1 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 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 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 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 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;... B = [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;... 0 0 0 0;...
1/m 0 0 0;... 1/m 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 1/Ix 0 0;... 0 1/Ix 0 0;...
0 0 1/Iy 0;... 0 0 1/Iy 0;...
0 0 0 1/Iz]; 0 0 0 1/Iz];
C = [1 0 0 0 0 0 0 0 0 0 0 0;...
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 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 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 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 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); x0 = 0;
y0 = 0;
z0 = 0;
xdot0 = 0;
ydot0 = 0;
zdot0 = 0;
phi0 = 10*(pi/180);
theta0 = 10*(pi/180);
psi0 = 0;
phidot0 = 0;
thetadot0 = 0;
psidot0 = 0;
initialCondition = [x0, y0, z0, xdot0, ydot0, zdot0, phi0, theta0, psi0, phidot0, thetadot0, psidot0];
%Gains
kpp = 10;
kdp = 0.2;
kpt = 4;
kdt = 0.2;
kpps = 1;
kdps = .4;
kpz = 100;
kdz = 20;

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