*** empty log message ***

This commit is contained in:
Antoine Drouin
2007-08-02 22:41:46 +00:00
parent 845ec5af04
commit 16cc2fd725
2 changed files with 114 additions and 67 deletions
+57 -61
View File
@@ -8,97 +8,93 @@ clear();
getf('baro_utils.sci');
getf('ekf.sci');
filename = "data/07_07_26__16_37_09.baro.txt";
[time, gps_alt, pressure, gps_climb, temp] = baro_read_log(filename);
filename = "data/07_08_02__14_57_30.data";
[time_pressure, pressure, time_altitude, altitude] = baro_read_pprz_log(filename);
//[time, gps_alt, pressure, gps_climb, temp] = baro_read_log(filename);
predict_only = 1;
dt = (time(length(time)) - time(1)) / length(time)
//
// Initialisation
//
[alt, a, b] = filter_init(10, pressure, gps_alt)
time_start = 110.;
time_end = 250.;
[pressure0,end_pressure, altitude0, end_altitude, a0, b0] = filter_init_timed(time_start, time_end, time_pressure, pressure, time_altitude, altitude)
X0 = [ alt; a; b ];
P0 = [ 1. 0. 0.
0. 1. 0.
0. 0. 1. ];
X0 = [ altitude0; a0];
P0 = [ 1. 0.
0. 2. ];
X = [X0];
P = [P0];
time_state = [time_pressure(end_pressure)];
//
// Iterations
//
for i=2:length(gps_alt)
// initial state
X0 = X(:, i-1);
// initial covariance
P0 = baro_get_P(P, i-1);
// command
pdot = (pressure(i) - pressure(i-1))/dt;
climb = pdot * X0(2);
// time derivative of state
X0dot = [ climb; 0; 0];
// Jacobian of Xdot wrt X
F = [ 0 pdot 0
0 0 0
0 0 0 ];
// process covariance noise
Q = [10. 0. 0.
0. .1 0.
0. 0. 0.1 ];
idx_a = end_altitude;
idx_s = 2;
for idx_p=(end_pressure+1):length(time_pressure)
[Xpred, Ppred] = ekf_predict_continuous(X0, X0dot, dt, P0, F, Q);
if ( predict_only )
X = [X Xpred];
P = [P Ppred];
else
// measurement GPS
measure = gps_alt(i);
err = measure - Xpred(1);
// Jacobian of measurement wrt X
H = [ 1 pressure(i) 1];
// Measurement covariance noise
R = 10.;
[Xup, Pup] = ekf_update(Xpred, Ppred, H, R, err);
// prediction
// initial state
X0 = X(:, idx_s-1);
// initial covariance
P0 = baro_get_P(P, idx_s-1);
// command
delta_p = pressure(idx_p) - pressure(idx_p-1);
delta_z = X0(2) * delta_p;
X1 = X0 + [delta_z; 0];
// jacobian
F = [ 1. delta_p
0 1. ];
// process covariance noise
Q = [ 1e-5 0.
0. 1e-7 ];
P1 = F*P0*F' + Q;
// update
err = altitude(idx_a) - X1(1);
H = [1 0];
R = 10;
E = H * P1 * H' + R;
K = P1 * H' * inv(E);
P2 = P1 - K * H * P1;
X2 = X1 + K * err;
X = [X X2];
P = [P P2];
time_state = [time_state time_pressure(idx_p)];
idx_p = idx_p + 1;
idx_s = idx_s + 1;
while ((idx_p < length(time_pressure)) & ...
(time_altitude(idx_a) < time_pressure(idx_p)) & ...
(idx_a < length(time_altitude))), idx_a = idx_a + 1; end
// measurement pressure
measure = pressure(i);
err
X = [X Xup];
P = [P Pup];
end
end
//
// Display
//
xbasc();
subplot(4,1,1)
xtitle('altitude');
plot2d([time; time]', [gps_alt; X(1,:)]', style=[5, 3], leg="gps@estimate");
plot2d([time_altitude]', [altitude]', style=[5], leg="gps");
plot2d([time_state]', [X(1,:)]', style=[3], leg="est_alt");
subplot(4,1,2)
xtitle('a');
plot2d([time]', [X(2,:)]', style=[5], leg="a");
xtitle('pressure');
plot2d([time_pressure]', [pressure]', style=[5], leg="pressure");
subplot(4,1,3)
xtitle('b');
plot2d([time]', [X(3,:)]', style=[5], leg="b");
xtitle('a');
plot2d([time_state]', [X(2,:)]', style=[5], leg="a");
subplot(4,1,4)
xtitle('covariance');
P11 = [];
P22 = [];
P33 = [];
for i=1:length(time)
for i=1:length(time_state)
Pi = baro_get_P(P, i);
P11 = [P11 Pi(1,1)];
P22 = [P22 Pi(2,2)];
P33 = [P33 Pi(3,3)];
end
plot2d([time; time; time]', [P11; P22; P33]', style=[5 3 2], leg="alt@a@b");
plot2d([time_state; time_state]', [P11; P22]', style=[5 3], leg="Palt@Pa");
+57 -6
View File
@@ -24,10 +24,12 @@ endfunction
function [time_pres, pres] = baro_read_pprz_log(filename)
function [time_pressure, pressure, time_gps, altitude] = baro_read_pprz_log(filename)
time_pres= [];
pres = [];
time_pressure= [];
pressure = [];
time_gps = [];
altitude = [];
u=mopen(filename, 'r');
while meof(u) == 0,
@@ -35,10 +37,16 @@ while meof(u) == 0,
if (line == "") continue end
[nb_scan, tip, ac, pr, te] = msscanf(1, line, '%f %d BARO_MS5534A %d %d');
if (nb_scan == 4)
time_pres = [time_pres tip];
pres = [pres pr];
time_pressure = [time_pressure tip];
pressure = [pressure pr];
else
[nb_scan, tig, ac, gmod, gue, gun, gcour, galt, gspeed, gclimb, gitow, guzone, gnerr] = ...
msscanf(1, line, '%f %d GPS %d %d %d %d %d %d %d %d %d %d');
if (nb_scan == 12)
time_gps = [time_gps tig];
altitude = [altitude galt];
end
end
end
mclose(u);
endfunction
@@ -122,6 +130,49 @@ function [pres, alt, a, b] = filter_init(avg_len, pressure, gps_alt)
endfunction
function [pressure0,end_pressure, altitude0, end_altitude, a0, b0] = filter_init_timed(time_start, time_end, time_pressure, pressure, time_altitude, altitude)
[avg_pressure, start_pressure, end_pressure] = average_period(time_start, time_end, time_pressure, pressure);
[avg_altitude, start_altitude, end_altitude] = average_period(time_start, time_end, time_altitude, altitude);
if (avg_pressure > 1030.0)
a0 = -16380. / 2^11;
elseif (avg_pressure > 970.0)
a0 = -17200. / 2^11;
elseif (avg_pressure > 920.0)
a0 = -18020. / 2^11;
elseif (avg_pressure > 850.0)
a0 = -19050. / 2^11;
elseif (avg_pressure > 780.0)
a0 = -20330. / 2^11;
elseif (avg_pressure > 710.0)
a0 = -21880. / 2^11;
elseif (avg_pressure > 650.0)
a0 = -23590. / 2^11;
end;
pressure0 = avg_pressure;
altitude0 = avg_altitude;
b0 = avg_altitude - a0 * avg_pressure;
endfunction
function [average, idx_start, idx_end] = average_period(time_start, time_end, time_samples, samples)
idx_start = 1;
while ((time_samples(idx_start) < time_start) & (idx_start <= length(time_samples))),
idx_start = idx_start+1;
end
idx_end = idx_start;
while ((time_samples(idx_end) < time_end) & (idx_end <= length(time_samples))),
idx_end = idx_end+1;
end
average = sum(samples(idx_start:idx_end), 'c') / (idx_end - idx_start);
endfunction
function [Pi] = baro_get_P(P, i)