initial commit

This commit is contained in:
2022-08-05 08:23:25 +03:00
commit 5ecdc6abcf
387 changed files with 3010095 additions and 0 deletions

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clear all;
close all;
% load their stereo parameters
% looks like they used the matlab calibration tool to get it.
% https://www.mathworks.com/help/vision/ref/stereoparameters.html#d117e94134
load ../raw/stereoParams.mat
%stereoParams = toStruct(stereoParams);
% transform between the left (stereo pair base) and the right camera
% the units of the stereo parameters are millimeters
% need to get R_1to2 and p_1in2
R_2to1 = stereoParams.RotationOfCamera2;
p_2in1 = stereoParams.TranslationOfCamera2'/1000;
T_LtoR = [...
R_2to1' p_2in1;
0 0 0 1
];
% T_LtoR = zeros(4,4);
% T_LtoR(1,1) = 1;
% T_LtoR(1,4) = -0.4751;
% T_LtoR(2,2) = 1;
% T_LtoR(3,3) = 1;
% T_LtoR(4,4) = 1;
% Vehicle2Stereo.txt
% Stereo camera (based on left camera) extrinsic calibration parameter from vehicle
% WHAT????? THEIR POSITION IS INCORRECTLY THE OPOSITE
% DIRECTION????!@#!@#?!@#!@#$!@$%!#@%!#%!~@%!@#%@!#^%#@%^!@#%@#%
p_LinV = [1.66944; 0.278027; 1.61215];
R_LtoV = [-0.00413442 -0.0196634 0.999798; -0.999931 -0.0109505 -0.00435034; 0.0110338 -0.999747 -0.0196168];
T_VtoL = [...
R_LtoV' -R_LtoV'*p_LinV;
0 0 0 1
];
% Vehicle2IMU.txt
% IMU extrinsic calibration parameter from vehicle
p_IinV = [-0.07; 0; 1.7];
R_ItoV = [1 0 0; 0 1 0; 0 0 1];
T_VtoI = [...
R_ItoV' -R_ItoV'*p_IinV;
0 0 0 1
];
% calculate the transform between the camneras and the IMU
T_LtoI = T_VtoI*inv(T_VtoL);
T_RtoI = T_VtoI*inv(T_LtoR*T_VtoL);
% print it out
fprintf('T_C0toI = \n');
fprintf('%.5f,%.5f,%.5f,%.5f,\n',T_LtoI(1,1),T_LtoI(1,2),T_LtoI(1,3),T_LtoI(1,4));
fprintf('%.5f,%.5f,%.5f,%.5f,\n',T_LtoI(2,1),T_LtoI(2,2),T_LtoI(2,3),T_LtoI(2,4));
fprintf('%.5f,%.5f,%.5f,%.5f,\n',T_LtoI(3,1),T_LtoI(3,2),T_LtoI(3,3),T_LtoI(3,4));
fprintf('%.5f,%.5f,%.5f,%.5f\n',T_LtoI(4,1),T_LtoI(4,2),T_LtoI(4,3),T_LtoI(4,4));
fprintf('T_C1toI = \n');
fprintf('%.5f,%.5f,%.5f,%.5f,\n',T_RtoI(1,1),T_RtoI(1,2),T_RtoI(1,3),T_RtoI(1,4));
fprintf('%.5f,%.5f,%.5f,%.5f,\n',T_RtoI(2,1),T_RtoI(2,2),T_RtoI(2,3),T_RtoI(2,4));
fprintf('%.5f,%.5f,%.5f,%.5f,\n',T_RtoI(3,1),T_RtoI(3,2),T_RtoI(3,3),T_RtoI(3,4));
fprintf('%.5f,%.5f,%.5f,%.5f\n',T_RtoI(4,1),T_RtoI(4,2),T_RtoI(4,3),T_RtoI(4,4));

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% clear and close old
close all;
clear all;
% our data file
path_main = '../';
filename_in = 'raw/urban39_global_pose.csv';
filename_out = 'urban39';
%% Vehicle2IMU.txt
% IMU extrinsic calibration parameter from vehicle
% The groundtruth poses are in the vehicle frame while we need the imu
p_IinV = [-0.07; 0; 1.7];
R_ItoV = [1 0 0; 0 1 0; 0 0 1];
T_VtoI = [...
R_ItoV' -R_ItoV'*p_IinV;
0 0 0 1
];
%% Load the groundtruth file
disp('Loading groundtruth...')
data_e = {};
data_e{length(data_e)+1} = importdata([path_main,filename_in],',',1);
temp_data = data_e{end}.data;
data_e{length(data_e)}.data = zeros(size(temp_data,1),8);
for jj=1:size(temp_data,1)
% timestamp is in nanoseconds so convert to our seconds
data_e{length(data_e)}.data(jj,1) = 1e-9*temp_data(jj,1);
% next get our transform
T_VtoUTM = [temp_data(jj,2:5); temp_data(jj,6:9); temp_data(jj,10:13); 0 0 0 1];
T_ItoUTM = T_VtoUTM*inv(T_VtoI);
% store in our vector
data_e{length(data_e)}.data(jj,2:4) = T_ItoUTM(1:3,4)';
data_e{length(data_e)}.data(jj,5:8) = rot2quat(T_ItoUTM(1:3,1:3)');
end
% finally write groundtruth data
fprintf('Outputing groundtruth (RPE format)...\n')
filename = [path_main,filename_out,'.txt'];
file = fopen([filename], 'w');
for t=1:size(data_e{end}.data(:,1:8),1)
fprintf(file, '%0.9f %0.6f %0.6f %0.6f %0.8f %0.8f %0.8f %0.8f\n',data_e{end}.data(t,1:8));
end
fprintf(' + saved %s\n',filename)
% finally write groundtruth data
fprintf('Outputing groundtruth (ETH format)...\n')
filename = [path_main,filename_out,'.csv'];
file = fopen([filename], 'w');
for t=1:size(data_e{end}.data(:,1:8),1)
fprintf(file, '%0.9f,%0.6f,%0.6f,%0.6f,%0.8f,%0.8f,%0.8f,%0.8f\n',1e9*data_e{end}.data(t,1),data_e{end}.data(t,2:4),data_e{end}.data(t,8),data_e{end}.data(t,5:7));
end
fprintf(' + saved %s\n',filename)

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function q = rot_matrix_to_quaternion(R)
% converts a rotational matrix to a unit quaternion, according to JPL
% procedure (Breckenridge Memo)
T = trace(R);
[dummy maxpivot] = max([R(1,1) R(2,2) R(3,3) T]);
switch maxpivot
case 1
q(1) = sqrt((1+2*R(1,1)-T)/4);
q(2:4) = 1/(4*q(1)) * [R(1,2)+R(2,1);
R(1,3)+R(3,1);
R(2,3)-R(3,2) ];
case 2
q(2) = sqrt((1+2*R(2,2)-T)/4);
q([1 3 4]) = 1/(4*q(2)) * [R(1,2)+R(2,1);
R(2,3)+R(3,2);
R(3,1)-R(1,3) ];
case 3
q(3) = sqrt((1+2*R(3,3)-T)/4);
q([1 2 4]) = 1/(4*q(3)) * [R(1,3)+R(3,1);
R(2,3)+R(3,2);
R(1,2)-R(2,1) ];
case 4
q(4) = sqrt((1+T)/4);
q(1:3) = 1/(4*q(4)) * [R(2,3)-R(3,2);
R(3,1)-R(1,3);
R(1,2)-R(2,1) ];
end % switch
% make column vector
q = q(:);
% 4th element is always positive
if q(4)<0
q = -q;
end
% quaternion normalization
q = q/sqrt(q'*q);