Kalman Filter - Can someone help me with to find the bug in my program?

Hello everybody, I am trying to implement the Kalman filter. I found a really good paper, which gives me all the equations I need. However I am not quite sure what value should n have (second equation 9.a) ?
Can someone help me with this?
My code is the following:
%% Kalman Filter
% Parameters
x1 = 1;
x2 = 1;
x3 = 1;
w = 0;
X = [x1, x2, x3];
alpha = 1;
n = 1;
k = 1;
lambda = alpha^2 *(n + k) - n;
betha = 1;
Q = 0;
roh = 1;
R = 0;
W_0_m = lambda / (lambda + n);
W_i = 1/(2*(lambda + n));
W_0_c = (lambda / (lambda + n)) + 1 - alpha^2 + betha;
y_t(:,1) = e; % x-acceleration from the sensor
y_t(:,2) = g; % y-acceleration from the sensor
x_dach = zeros;
L = 200000; % length of the simulation
for z = 1:L
%% A priori estimation
[X_est(1,1), X_est(2,1), X_est(3,1)] = stateequation(X(1), X(2), X(3), w);
for i = 0: 2*n
if i == 0
x_t_dach_m = W_0_m * X_est(i+1);
else
x_t_dach_m = W_i * X_est(i+1)+ x_t_dach_m;
end
end
for j = 0: 2*n
if i== 0
P_t_m = W_0_c * (X_est(i+1)-x_t_dach_m) * (X_est(i+1)-x_t_dach_m);
else
P_t_m = W_i * (X_est(i+1)-x_t_dach_m) * (X_est(i+1)-x_t_dach_m) + P_t_m;
end
end
P_t_m = P_t_m + Q;
X_t_t1 = [x_t_dach_m, x_t_dach_m + gamma * sqrt(P_t_m), x_t_dach_m - gamma * sqrt(P_t_m)];
Y_t_t1 = outputtransformation(X_t_t1(1), X_t_t1(2), roh, v);
for i = 0: 2*n
if i == 0
y_t_dach_m = W_0_m * Y_t_t1(i+1);
else
y_t_dach_m = W_i * Y_t_t1(i+1) + y_t_dach_m;
end
end
%% A posteriori estimation
for i = 0:2*n
if i == 0
Py_y = W_0_c * (Y_t_t1(i+1)-y_t_dach_m) * (Y_t_t1(i+1)-y_t_dach_m);
else
Py_y = W_i * (Y_t_t1(i+1)-y_t_dach_m) * (Y_t_t1(i+1)-y_t_dach_m) + Py_y;
end
end
Py_y = Py_y + R;
for i = 0:2*n
if i == 0
Px_y = W_0_c * (X_t_t1(i+1)-x_t_dach_m) * (X_t_t1(i+1)-x_t_dach_m);
else
Px_y = W_i * (X_t_t1(i+1)-x_t_dach_m) * (X_t_t1(i+1)-x_t_dach_m) + Px_y;
end
end
K_t = Px_y * inv(Py_y);
x_dach(z) = x_t_dach_m + K_t * (y_t - y_t_dach_m);
P_t = P_t_m - K_t * Py_y * K_t;
X = X_t_t1;
end
%% Functions
function [x1_new, x2_new, x3_new] = stateequation (x1, x2, x3, w)
x1_new = 2*cos(x3) * x1 -x2;
x2_new = x1;
x3_new = x3 + w;
end
function y_new = outputtransformation (x1, x2, roh, v)
y_new = -(1 + roh^2) * x1 + roh^2 * x2 + v;
end

3 Comments

Original question on 7th November 2020 by [original poster] retrieved from Google Cache:
Kalman Filter - Can someone help me with to find the bug in my program?
Hello everybody, I am trying to implement the Kalman filter. I found a really good paper, which gives me all the equations I need. However I am not quite sure what value should n have (second equation 9.a) ?
Can someone help me with this?
My code is the following:
%% Kalman Filter
% Parameters
x1 = 1;
x2 = 1;
x3 = 1;
w = 0;
X = [x1, x2, x3];
alpha = 1;
n = 1;
k = 1;
lambda = alpha^2 *(n + k) - n;
betha = 1;
Q = 0;
roh = 1;
R = 0;
W_0_m = lambda / (lambda + n);
W_i = 1/(2*(lambda + n));
W_0_c = (lambda / (lambda + n)) + 1 - alpha^2 + betha;
y_t(:,1) = e; % x-acceleration from the sensor
y_t(:,2) = g; % y-acceleration from the sensor
x_dach = zeros;
L = 200000; % length of the simulation
for z = 1:L
%% A priori estimation
[X_est(1,1), X_est(2,1), X_est(3,1)] = stateequation(X(1), X(2), X(3), w);
for i = 0: 2*n
if i == 0
x_t_dach_m = W_0_m * X_est(i+1);
else
x_t_dach_m = W_i * X_est(i+1)+ x_t_dach_m;
end
end
for j = 0: 2*n
if i== 0
P_t_m = W_0_c * (X_est(i+1)-x_t_dach_m) * (X_est(i+1)-x_t_dach_m);
else
P_t_m = W_i * (X_est(i+1)-x_t_dach_m) * (X_est(i+1)-x_t_dach_m) + P_t_m;
end
end
P_t_m = P_t_m + Q;
X_t_t1 = [x_t_dach_m, x_t_dach_m + gamma * sqrt(P_t_m), x_t_dach_m - gamma * sqrt(P_t_m)];
Y_t_t1 = outputtransformation(X_t_t1(1), X_t_t1(2), roh, v);
for i = 0: 2*n
if i == 0
y_t_dach_m = W_0_m * Y_t_t1(i+1);
else
y_t_dach_m = W_i * Y_t_t1(i+1) + y_t_dach_m;
end
end
%% A posteriori estimation
for i = 0:2*n
if i == 0
Py_y = W_0_c * (Y_t_t1(i+1)-y_t_dach_m) * (Y_t_t1(i+1)-y_t_dach_m);
else
Py_y = W_i * (Y_t_t1(i+1)-y_t_dach_m) * (Y_t_t1(i+1)-y_t_dach_m) + Py_y;
end
end
Py_y = Py_y + R;
for i = 0:2*n
if i == 0
Px_y = W_0_c * (X_t_t1(i+1)-x_t_dach_m) * (X_t_t1(i+1)-x_t_dach_m);
else
Px_y = W_i * (X_t_t1(i+1)-x_t_dach_m) * (X_t_t1(i+1)-x_t_dach_m) + Px_y;
end
end
K_t = Px_y * inv(Py_y);
x_dach(z) = x_t_dach_m + K_t * (y_t - y_t_dach_m);
P_t = P_t_m - K_t * Py_y * K_t;
X = X_t_t1;
end
%% Functions
function [x1_new, x2_new, x3_new] = stateequation (x1, x2, x3, w)
x1_new = 2*cos(x3) * x1 -x2;
x2_new = x1;
x3_new = x3 + w;
end
function y_new = outputtransformation (x1, x2, roh, v)
y_new = -(1 + roh^2) * x1 + roh^2 * x2 + v;
end
@HF You are allowed to ask for removal of your name from a post (I have so often seen Mathworks staff do this, that I have taken the liberty of removing it from Stephen's post).
However, it is extremely rude to remove your question. Why should your rudeness be answered by civility? Please don't edit away your question after someone has spent the time answering it.

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Answers (1)

The program never assigns e and g, so it fails at that point. You need to assign them some values.

2 Comments

Hi thanks for your advice! e and g are already assigned in the workspace
If you still have problems, then post the missing code where these other variables are mysteriously put into the workspace. Otherwise people can't run your code and reproduce your error(s).

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Asked:

HF
on 7 Nov 2020

Commented:

on 6 May 2021

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