open source pkg v1
This commit is contained in:
Vijay Yadev
9
pkg/OpenFace/matlab_version/PDM_helpers/AddOrthRow.m
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9
pkg/OpenFace/matlab_version/PDM_helpers/AddOrthRow.m
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function [RotFull] = AddOrthRow(RotSmall)
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% We can work out these values from the small version of the rotation matrix Rx * Ry * Rz (if you plug in values you can work it out, just slightly tedious)
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RotFull = zeros(3,3);
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RotFull(1:2, :) = RotSmall;
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RotFull(3,1) = RotSmall(1, 2) * RotSmall(2, 3) - RotSmall(1, 3) * RotSmall(2, 2);
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RotFull(3,2) = RotSmall(1, 3) * RotSmall(2, 1) - RotSmall(1, 1) * RotSmall(2, 3);
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RotFull(3,3) = RotSmall(1, 1) * RotSmall(2, 2) - RotSmall(1, 2) * RotSmall(2, 1);
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22
pkg/OpenFace/matlab_version/PDM_helpers/AlignShapesKabsch.m
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22
pkg/OpenFace/matlab_version/PDM_helpers/AlignShapesKabsch.m
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function [ R, T ] = AlignShapesKabsch ( alignFrom, alignTo )
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%ALIGN3DSHAPES Summary of this function goes here
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% Detailed explanation goes here
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dims = size(alignFrom, 2);
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alignFromMean = alignFrom - repmat(mean(alignFrom), size(alignFrom,1),1);
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alignToMean = alignTo - repmat(mean(alignTo), size(alignTo,1),1);
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[U, ~, V] = svd( alignFromMean' * alignToMean);
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% make sure no reflection is there
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d = sign(det(V*U'));
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corr = eye(dims);
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corr(end,end) = d;
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R = V*corr*U';
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T = mean(alignTo) - (R * mean(alignFrom)')';
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T = T';
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end
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@@ -0,0 +1,30 @@
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function [ A, T, error, alignedShape ] = AlignShapesWithScale( alignFrom, alignTo )
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%ALIGNSHAPESWITHSCALE Summary of this function goes here
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% Detailed explanation goes here
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numPoints = size(alignFrom,1);
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meanFrom = mean(alignFrom);
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meanTo = mean(alignTo);
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alignFromMeanNormed = bsxfun(@minus, alignFrom, meanFrom);
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alignToMeanNormed = bsxfun(@minus, alignTo, meanTo);
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% scale now
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sFrom = sqrt(sum(alignFromMeanNormed(:).^2)/numPoints);
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sTo = sqrt(sum(alignToMeanNormed(:).^2)/numPoints);
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s = sTo / sFrom;
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alignFromMeanNormed = alignFromMeanNormed/sFrom;
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alignToMeanNormed = alignToMeanNormed/sTo;
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[R, t] = AlignShapesKabsch(alignFromMeanNormed, alignToMeanNormed);
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A = s * R;
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aligned = (A * alignFrom')';
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T = mean(alignTo - aligned);
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alignedShape = bsxfun(@plus, aligned, T);
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error = sqrt(mean(sum((alignedShape - alignTo).^2,2)));
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end
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11
pkg/OpenFace/matlab_version/PDM_helpers/AxisAngle2Rot.m
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11
pkg/OpenFace/matlab_version/PDM_helpers/AxisAngle2Rot.m
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function [Rot] = AxisAngle2Rot(axisAngle)
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theta = norm(axisAngle, 2);
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nx = axisAngle / theta;
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nx = [ 0 -nx(3) nx(2);
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nx(3) 0 -nx(1);
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-nx(2) nx(1) 0 ];
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Rot = eye(3) + sin(theta) * nx + (1-cos(theta))*nx^2;
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11
pkg/OpenFace/matlab_version/PDM_helpers/Euler2Rot.m
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11
pkg/OpenFace/matlab_version/PDM_helpers/Euler2Rot.m
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function [Rot] = Euler2Rot(euler)
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rx = euler(1);
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ry = euler(2);
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rz = euler(3);
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Rx = [1 0 0; 0 cos(rx) -sin(rx); 0 sin(rx) cos(rx)];
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Ry = [cos(ry) 0 sin(ry); 0 1 0; -sin(ry) 0 cos(ry)];
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Rz = [cos(rz) -sin(rz) 0; sin(rz) cos(rz) 0; 0 0 1];
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Rot = Rx * Ry * Rz;
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7
pkg/OpenFace/matlab_version/PDM_helpers/GetShape3D.m
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7
pkg/OpenFace/matlab_version/PDM_helpers/GetShape3D.m
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function [shape3D] = GetShape3D(M, V, p)
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shape3D = M + V * p;
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shape3D = reshape(shape3D, numel(shape3D) / 3, 3);
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end
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20
pkg/OpenFace/matlab_version/PDM_helpers/GetShapeOrtho.m
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20
pkg/OpenFace/matlab_version/PDM_helpers/GetShapeOrtho.m
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function [shape2D] = GetShapeOrtho(M, V, p, global_params)
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% M - mean shape vector
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% V - eigenvectors
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% p - parameters of non-rigid shape
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% V_exp
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% p_exp
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% global_params includes scale, euler rotation, translation,
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% R - rotation matrix
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% T - translation vector (tx, ty)
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R = Euler2Rot(global_params(2:4));
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T = [global_params(5:6); 0];
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a = global_params(1);
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shape3D = GetShape3D(M, V, p);
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shape2D = bsxfun(@plus, a * R*shape3D', T);
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shape2D = shape2D';
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end
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103
pkg/OpenFace/matlab_version/PDM_helpers/ProcrustesAnalysis.m
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103
pkg/OpenFace/matlab_version/PDM_helpers/ProcrustesAnalysis.m
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function [normX, normY, meanShape, Transform] = ProcrustesAnalysis(x, y, options)
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% Translate all elements to origin and scale to 1
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normX = zeros(size(x));
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normY = zeros(size(y));
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for i = 1:size(x,1)
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offsetX = mean(x(i,:));
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offsetY = mean(y(i,:));
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Transform.offsetX(i) = offsetX;
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Transform.offsetY(i) = offsetY;
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normX(i,:) = x(i,:) - offsetX;
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normY(i,:) = y(i,:) - offsetY;
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% Get the Frobenius norm, to scale the shapes to unit size
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scale = norm([normX(i,:) normY(i,:)], 'fro');
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Transform.scale(i) = scale;
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normX(i,:) = normX(i,:)/scale;
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normY(i,:) = normY(i,:)/scale;
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end
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% Rotate elements untill all of them have the same orientation
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% the initial estimate of rotation would be the first element
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% if change is less than 1% stop (shouldn't take more than 2 steps)
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change = 0.1;
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meanShape = [ normX(1,:); normY(1,:) ]';
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Transform.Rotation = zeros(size(x,1),1);
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for i = 1:30
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% align all of the shapes to the mean shape
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% remember all orientations to get the mean one
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orientations = zeros(size(normX,1),1);
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for j = 1:size(x,1)
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% do SVD of mean * X'
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currentShape = [ normX(j,:); normY(j,:) ]';
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[U, ~, V] = svd( meanShape' * currentShape);
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rot = V*U';
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if(asin(rot(2,1)) > 0)
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orientations(j) = real(acos(rot(1,1)));
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else
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orientations(j) = real(-acos(rot(1,1)));
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end
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Transform.Rotation(j) = Transform.Rotation(j) + orientations(j);
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currentShape = currentShape * rot;
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normX(j,:) = currentShape(:,1)';
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normY(j,:) = currentShape(:,2)';
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end
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% recalculate the mean shape;
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oldMean = meanShape;
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meanShape = [mean(normX); mean(normY)]';
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% rotate the mean shape to mean rotation
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meanOrientation = mean(orientations);
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% Do this only the first time
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if(i==1)
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rotM = [ cos(-meanOrientation) -sin(-meanOrientation); sin(-meanOrientation) cos(-meanOrientation) ];
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meanShape = meanShape * rotM;
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end
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% scale mean shape to unit
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meanScale = norm(meanShape, 'fro');
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meanShape = meanShape*(1/meanScale);
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% find frobenious norm
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diff = norm(oldMean - meanShape, 'fro');
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if(diff/norm(oldMean,'fro') < change)
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break;
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end
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end
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% transform to tangent space to preserve linearities
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% get the scaling factors for each shape
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if(options.TangentSpaceTransform)
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scaling = [ normX normY ] * [ meanShape(:,1)' meanShape(:,2)']';
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for i=1:size(x,1)
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normX(i,:) = normX(i,:) * (1 / scaling(i));
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normY(i,:) = normY(i,:) * (1 / scaling(i));
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end
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end
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139
pkg/OpenFace/matlab_version/PDM_helpers/ProcrustesAnalysis3D.m
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139
pkg/OpenFace/matlab_version/PDM_helpers/ProcrustesAnalysis3D.m
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function [ normX, normY, normZ, meanShape, Transform ] = ProcrustesAnalysis3D( x, y, z, tangentSpace, meanShape )
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%PROCRUSTESANALYSIS3D Summary of this function goes here
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% Detailed explanation goes here
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meanProvided = false;
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if(nargin > 4)
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meanProvided = true;
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end
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% Translate all elements to origin
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normX = zeros(size(x));
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normY = zeros(size(y));
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normZ = zeros(size(z));
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for i = 1:size(x,1)
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offsetX = mean(x(i,:));
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offsetY = mean(y(i,:));
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offsetZ = mean(z(i,:));
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Transform.offsetX(i) = offsetX;
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Transform.offsetY(i) = offsetY;
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Transform.offsetZ(i) = offsetZ;
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normX(i,:) = x(i,:) - offsetX;
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normY(i,:) = y(i,:) - offsetY;
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normZ(i,:) = z(i,:) - offsetZ;
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end
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% Rotate elements untill all of them have the same orientation
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% the initial estimate of rotation would be the first element
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% if change is less than 1% stop (shouldn't take more than 2 steps)
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change = 0.1;
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if(~meanProvided)
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meanShape = [ mean(normX); mean(normY); mean(normZ) ]';
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end
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% scale all the shapes to mean shape
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% Get the Frobenius norm, to scale the shapes to mean size (still want to
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% retain mm)
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meanScale = norm(meanShape, 'fro');
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for i = 1:size(x,1)
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scale = norm([normX(i,:) normY(i,:) normZ(i,:)], 'fro')/meanScale;
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normX(i,:) = normX(i,:)/scale;
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normY(i,:) = normY(i,:)/scale;
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normZ(i,:) = normZ(i,:)/scale;
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end
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Transform.RotationX = zeros(size(x,1),1);
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Transform.RotationY = zeros(size(x,1),1);
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Transform.RotationZ = zeros(size(x,1),1);
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for i = 1:30
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% align all of the shapes to the mean shape
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% remember all orientations to get the mean one (in euler angle form, pitch, yaw roll)
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orientationsX = zeros(size(normX,1),1);
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orientationsY = zeros(size(normX,1),1);
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orientationsZ = zeros(size(normX,1),1);
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for j = 1:size(x,1)
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currentShape = [normX(j,:); normY(j,:); normZ(j,:)]';
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% we want to align the current shape to the mean one
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[ R, T ] = AlignShapesKabsch(currentShape, meanShape);
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eulers = Rot2Euler(R);
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orientationsX(j) = eulers(1);
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orientationsY(j) = eulers(2);
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orientationsZ(j) = eulers(3);
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Transform.RotationX(j) = eulers(1);
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Transform.RotationY(j) = eulers(2);
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Transform.RotationZ(j) = eulers(3);
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currentShape = R * currentShape';
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normX(j,:) = currentShape(1,:);
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normY(j,:) = currentShape(2,:);
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normZ(j,:) = currentShape(3,:);
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end
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% recalculate the mean shape
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% if(~meanProvided)
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oldMean = meanShape;
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meanShape = [mean(normX); mean(normY); mean(normZ)]';
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meanScale = norm(meanShape, 'fro');
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% end
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for j = 1:size(x,1)
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scale = norm([normX(j,:) normY(j,:) normZ(j,:)], 'fro')/meanScale;
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normX(j,:) = normX(j,:)/scale;
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normY(j,:) = normY(j,:)/scale;
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normZ(j,:) = normZ(j,:)/scale;
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end
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if(i==1 && ~meanProvided)
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% rotate the mean shape to mean rotation
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meanOrientationX = mean(orientationsX);
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meanOrientationY = mean(orientationsY);
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meanOrientationZ = mean(orientationsZ);
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R = Euler2Rot([meanOrientationX, meanOrientationY, meanOrientationZ]);
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meanShape = (R * meanShape')';
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end
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% find frobenious norm
|
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diff = norm(oldMean - meanShape, 'fro');
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|
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if(diff/norm(oldMean,'fro') < change)
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break;
|
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end
|
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|
||||
end
|
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|
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% transform to tangent space to preserve linearities
|
||||
|
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% get the scaling factors for each shape
|
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if(tangentSpace)
|
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[ normX, normY, normZ] = TangentSpaceTransform(normX, normY, normZ, meanShape);
|
||||
end
|
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|
||||
end
|
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11
pkg/OpenFace/matlab_version/PDM_helpers/Rot2AxisAngle.m
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11
pkg/OpenFace/matlab_version/PDM_helpers/Rot2AxisAngle.m
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@@ -0,0 +1,11 @@
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function [ axisAngle ] = Rot2AxisAngle( Rot )
|
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%ROT2AXISANGLE Summary of this function goes here
|
||||
% Detailed explanation goes here
|
||||
|
||||
theta = acos((trace(Rot) - 1) / 2);
|
||||
|
||||
vec = 1.0/(2*sin(theta));
|
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vec = vec * [Rot(3,2) - Rot(2,3), Rot(1,3) - Rot(3,1), Rot(2,1) - Rot(1,2)];
|
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axisAngle = vec * theta;
|
||||
end
|
||||
|
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12
pkg/OpenFace/matlab_version/PDM_helpers/Rot2Euler.m
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12
pkg/OpenFace/matlab_version/PDM_helpers/Rot2Euler.m
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@@ -0,0 +1,12 @@
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||||
function [euler] = Rot2Euler(R)
|
||||
|
||||
q0 = sqrt( 1 + R(1,1) + R(2,2) + R(3,3) ) / 2;
|
||||
q1 = (R(3,2) - R(2,3)) / (4*q0) ;
|
||||
q2 = (R(1,3) - R(3,1)) / (4*q0) ;
|
||||
q3 = (R(2,1) - R(1,2)) / (4*q0) ;
|
||||
|
||||
yaw = asin(2*(q0*q2 + q1*q3));
|
||||
pitch= atan2(2*(q0*q1-q2*q3), q0*q0-q1*q1-q2*q2+q3*q3);
|
||||
roll = atan2(2*(q0*q3-q1*q2), q0*q0+q1*q1-q2*q2-q3*q3);
|
||||
|
||||
euler = [pitch, yaw, roll];
|
||||
@@ -0,0 +1,17 @@
|
||||
function [ transformedX, transformedY, transformedZ ] = TangentSpaceTransform( x, y, z, meanShape )
|
||||
%TANGENTSPACETRANSFORM Summary of this function goes here
|
||||
% Detailed explanation goes here
|
||||
|
||||
scaling = [ x y z] * [ meanShape(:,1)' meanShape(:,2)' meanShape(:,3)']';
|
||||
for i=1:size(x,1)
|
||||
x(i,:) = x(i,:) * (1 / scaling(i));
|
||||
y(i,:) = y(i,:) * (1 / scaling(i));
|
||||
z(i,:) = z(i,:) * (1 / scaling(i));
|
||||
end
|
||||
|
||||
transformedX = x * mean(scaling);
|
||||
transformedY = y * mean(scaling);
|
||||
transformedZ = z * mean(scaling);
|
||||
|
||||
end
|
||||
|
||||
@@ -0,0 +1,345 @@
|
||||
function [ a, R, T, T3D, params, error, shapeOrtho ] = fit_PDM_ortho_proj_to_2D( M, E, V, shape2D, f, cx, cy)
|
||||
%FITPDMTO2DSHAPE Summary of this function goes here
|
||||
% Detailed explanation goes here
|
||||
|
||||
params = zeros(size(E));
|
||||
|
||||
hidden = false;
|
||||
|
||||
% if some of the points are unavailable modify M, V, and shape2D (can
|
||||
% later infer the actual shape from this)
|
||||
if(sum(shape2D(:)==0) > 0)
|
||||
|
||||
hidden = true;
|
||||
% which indices to remove
|
||||
inds_to_rem = shape2D(:,1) == 0 | shape2D(:,2) == 0;
|
||||
|
||||
shape2D = shape2D(~inds_to_rem,:);
|
||||
|
||||
inds_to_rem = repmat(inds_to_rem, 3, 1);
|
||||
|
||||
M_old = M;
|
||||
V_old = V;
|
||||
|
||||
M = M(~inds_to_rem);
|
||||
V = V(~inds_to_rem,:);
|
||||
|
||||
end
|
||||
|
||||
num_points = numel(M) / 3;
|
||||
|
||||
m = reshape(M, num_points, 3)';
|
||||
width_model = max(m(1,:)) - min(m(1,:));
|
||||
height_model = max(m(2,:)) - min(m(2,:));
|
||||
|
||||
bounding_box = [min(shape2D(:,1)), min(shape2D(:,2)),...
|
||||
max(shape2D(:,1)), max(shape2D(:,2))];
|
||||
|
||||
a = (((bounding_box(3) - bounding_box(1)) / width_model) + ((bounding_box(4) - bounding_box(2))/ height_model)) / 2;
|
||||
|
||||
tx = (bounding_box(3) + bounding_box(1))/2;
|
||||
ty = (bounding_box(4) + bounding_box(2))/2;
|
||||
|
||||
% correct it so that the bounding box is just around the minimum
|
||||
% and maximum point in the initialised face
|
||||
tx = tx - a*(min(m(1,:)) + max(m(1,:)))/2;
|
||||
ty = ty - a*(min(m(2,:)) + max(m(2,:)))/2;
|
||||
|
||||
R = eye(3);
|
||||
T = [tx; ty];
|
||||
|
||||
currShape = getShapeOrtho(M, V, params, R, T, a);
|
||||
|
||||
currError = getRMSerror(currShape, shape2D);
|
||||
|
||||
reg_rigid = zeros(6,1);
|
||||
regFactor = 20;
|
||||
regularisations = [reg_rigid; regFactor ./ E]; % the above version, however, does not perform as well
|
||||
regularisations = diag(regularisations)*diag(regularisations);
|
||||
|
||||
red_in_a_row = 0;
|
||||
|
||||
for i=1:1000
|
||||
|
||||
shape3D = M + V * params;
|
||||
shape3D = reshape(shape3D, numel(shape3D) / 3, 3);
|
||||
|
||||
% Now find the current residual error
|
||||
currShape = a * R(1:2,:)*shape3D' + repmat(T, 1, numel(M)/3);
|
||||
currShape = currShape';
|
||||
|
||||
error_res = shape2D - currShape;
|
||||
|
||||
eul = Rot2Euler(R);
|
||||
|
||||
p_global = [a; eul'; T];
|
||||
|
||||
% get the Jacobians
|
||||
J = CalcJacobian(M, V, params, p_global);
|
||||
|
||||
% RLMS style update
|
||||
p_delta = (J'*J + regularisations) \ (J'*error_res(:) - regularisations*[p_global;params]);
|
||||
|
||||
[params, p_global] = CalcReferenceUpdate(p_delta, params, p_global);
|
||||
|
||||
a = p_global(1);
|
||||
R = Euler2Rot(p_global(2:4));
|
||||
T = p_global(5:6);
|
||||
|
||||
shape3D = M + V * params;
|
||||
shape3D = reshape(shape3D, numel(shape3D) / 3, 3);
|
||||
currShape = a * R(1:2,:)*shape3D' + repmat(T, 1, numel(M)/3);
|
||||
currShape = currShape';
|
||||
|
||||
error = getRMSerror(currShape, shape2D);
|
||||
|
||||
if(0.999 * currError < error)
|
||||
red_in_a_row = red_in_a_row + 1;
|
||||
if(red_in_a_row == 5)
|
||||
break;
|
||||
end
|
||||
end
|
||||
|
||||
currError = error;
|
||||
|
||||
end
|
||||
|
||||
if(hidden)
|
||||
shapeOrtho = getShapeOrtho(M_old, V_old, params, R, T, a);
|
||||
else
|
||||
shapeOrtho = currShape;
|
||||
end
|
||||
if(nargin == 7)
|
||||
|
||||
Zavg = f / a;
|
||||
Xavg = (T(1) - cx) / a;
|
||||
Yavg = (T(2) - cy) / a;
|
||||
|
||||
T3D = [Xavg;Yavg;Zavg];
|
||||
else
|
||||
T3D = [0;0;0];
|
||||
end
|
||||
|
||||
end
|
||||
|
||||
function [shape2D] = getShapeOrtho(M, V, p, R, T, a)
|
||||
|
||||
% M - mean shape vector
|
||||
% V - eigenvectors
|
||||
% p - parameters of non-rigid shape
|
||||
% R - rotation matrix
|
||||
% T - translation vector (tx, ty)
|
||||
shape3D = getShape3D(M, V, p);
|
||||
shape2D = a * R(1:2,:)*shape3D' + repmat(T, 1, numel(M)/3);
|
||||
shape2D = shape2D';
|
||||
end
|
||||
|
||||
function [shape2D] = getShapeOrthoFull(M, V, p, R, T, a)
|
||||
|
||||
% M - mean shape vector
|
||||
% V - eigenvectors
|
||||
% p - parameters of non-rigid shape
|
||||
% R - rotation matrix
|
||||
% T - translation vector (tx, ty)
|
||||
T = [T; 0];
|
||||
shape3D = getShape3D(M, V, p);
|
||||
shape2D = a * R*shape3D' + repmat(T, 1, numel(M)/3);
|
||||
shape2D = shape2D';
|
||||
end
|
||||
|
||||
function [shape3D] = getShape3D(M, V, params)
|
||||
|
||||
shape3D = M + V * params;
|
||||
shape3D = reshape(shape3D, numel(shape3D) / 3, 3);
|
||||
|
||||
end
|
||||
|
||||
function [error] = getRMSerror(shape2Dv1, shape2Dv2)
|
||||
|
||||
error = sqrt(mean(reshape(shape2Dv1 - shape2Dv2, numel(shape2Dv1), 1).^2));
|
||||
|
||||
end
|
||||
|
||||
% This calculates the combined rigid with non-rigid Jacobian
|
||||
function J = CalcJacobian(M, V, p, p_global)
|
||||
|
||||
n = size(M, 1)/3;
|
||||
|
||||
non_rigid_modes = size(V,2);
|
||||
|
||||
J = zeros(n*2, 6 + non_rigid_modes);
|
||||
|
||||
|
||||
% now the layour is
|
||||
% ---------- Rigid part -------------------|----Non rigid part--------|
|
||||
% dx_1/ds, dx_1/dr1, ... dx_1/dtx, dx_1/dty dx_1/dp_1 ... dx_1/dp_m
|
||||
% dx_2/ds, dx_2/dr1, ... dx_2/dtx, dx_2/dty dx_2/dp_1 ... dx_2/dp_m
|
||||
% ...
|
||||
% dx_n/ds, dx_n/dr1, ... dx_n/dtx, dx_n/dty dx_n/dp_1 ... dx_n/dp_m
|
||||
% dy_1/ds, dy_1/dr1, ... dy_1/dtx, dy_1/dty dy_1/dp_1 ... dy_1/dp_m
|
||||
% ...
|
||||
% dy_n/ds, dy_n/dr1, ... dy_n/dtx, dy_n/dty dy_n/dp_1 ... dy_n/dp_m
|
||||
|
||||
% getting the rigid part
|
||||
J(:,1:6) = CalcRigidJacobian(M, V, p, p_global);
|
||||
|
||||
% constructing the non-rigid part
|
||||
R = Euler2Rot(p_global(2:4));
|
||||
s = p_global(1);
|
||||
|
||||
% 'rotate' and 'scale' the principal components
|
||||
|
||||
% First reshape to 3D
|
||||
V_X = V(1:n,:);
|
||||
V_Y = V(n+1:2*n,:);
|
||||
V_Z = V(2*n+1:end,:);
|
||||
|
||||
J_x_non_rigid = s*(R(1,1)*V_X + R(1,2)*V_Y + R(1,3)*V_Z);
|
||||
J_y_non_rigid = s*(R(2,1)*V_X + R(2,2)*V_Y + R(2,3)*V_Z);
|
||||
|
||||
J(1:n, 7:end) = J_x_non_rigid;
|
||||
J(n+1:end, 7:end) = J_y_non_rigid;
|
||||
|
||||
end
|
||||
|
||||
function J = CalcRigidJacobian(M, V, p, p_global)
|
||||
|
||||
n = size(M, 1)/3;
|
||||
|
||||
% Get the current 3D shape (not affected by global transform, as this
|
||||
% is how the Jacobian was derived (for derivation please see
|
||||
% ../derivations/orthoJacobian
|
||||
shape3D = GetShape3D(M, V, p);
|
||||
|
||||
% Get the rotation matrix corresponding to current global orientation
|
||||
R = Euler2Rot(p_global(2:4));
|
||||
s = p_global(1);
|
||||
|
||||
% Rigid Jacobian is laid out as follows
|
||||
% dx_1/ds, dx_1/dr1, dx_1/dr2, dx_1/dr3, dx_1/dtx, dx_1/dty
|
||||
% dx_2/ds, dx_2/dr1, dx_2/dr2, dx_2/dr3, dx_2/dtx, dx_2/dty
|
||||
% ...
|
||||
% dx_n/ds, dx_n/dr1, dx_n/dr2, dx_n/dr3, dx_n/dtx, dx_n/dty
|
||||
% dy_1/ds, dy_1/dr1, dy_1/dr2, dy_1/dr3, dy_1/dtx, dy_1/dty
|
||||
% ...
|
||||
% dy_n/ds, dy_n/dr1, dy_n/dr2, dy_n/dr3, dy_n/dtx, dy_n/dty
|
||||
|
||||
J = zeros(n*2, 6);
|
||||
|
||||
% dx/ds = X * r11 + Y * r12 + Z * r13
|
||||
% dx/dr1 = s*(r13 * Y - r12 * Z)
|
||||
% dx/dr2 = -s*(r13 * X - r11 * Z)
|
||||
% dx/dr3 = s*(r12 * X - r11 * Y)
|
||||
% dx/dtx = 1
|
||||
% dx/dty = 0
|
||||
|
||||
% dy/ds = X * r21 + Y * r22 + Z * r23
|
||||
% dy/dr1 = s * (r23 * Y - r22 * Z)
|
||||
% dy/dr2 = -s * (r23 * X - r21 * Z)
|
||||
% dy/dr3 = s * (r22 * X - r21 * Y)
|
||||
% dy/dtx = 0
|
||||
% dy/dty = 1
|
||||
|
||||
% set the Jacobian for x's
|
||||
|
||||
% with respect to scaling factor
|
||||
J(1:n,1) = shape3D * R(1,:)';
|
||||
|
||||
% with respect to angular rotation around x, y, and z axes
|
||||
|
||||
% Change of x with respect to change in axis angle rotation
|
||||
dxdR = [ 0, R(1,3), -R(1,2);
|
||||
-R(1,3), 0, R(1,1);
|
||||
R(1,2), -R(1,1), 0];
|
||||
|
||||
J(1:n,2:4) = s*(dxdR * shape3D')';
|
||||
|
||||
% with respect to translation
|
||||
J(1:n,5) = 1;
|
||||
J(1:n,6) = 0;
|
||||
|
||||
% set the Jacobian for y's
|
||||
|
||||
% with respect to scaling factor
|
||||
J(n+1:end,1) = shape3D * R(2,:)';
|
||||
|
||||
% with respect to angular rotation around x, y, and z axes
|
||||
|
||||
% Change of y with respect to change in axis angle rotation
|
||||
dydR = [ 0, R(2,3), -R(2,2);
|
||||
-R(2,3), 0, R(2,1);
|
||||
R(2,2), -R(2,1), 0];
|
||||
|
||||
J(n+1:end,2:4) = s*(dydR * shape3D')';
|
||||
|
||||
% with respect to translation
|
||||
J(n+1:end,5) = 0;
|
||||
J(n+1:end,6) = 1;
|
||||
|
||||
end
|
||||
|
||||
% This updates the parameters based on the updates from the RLMS
|
||||
function [non_rigid, rigid] = CalcReferenceUpdate(params_delta, current_non_rigid, current_global)
|
||||
|
||||
|
||||
rigid = zeros(6, 1);
|
||||
% Same goes for scaling and translation parameters
|
||||
rigid(1) = current_global(1) + params_delta(1);
|
||||
rigid(5) = current_global(5) + params_delta(5);
|
||||
rigid(6) = current_global(6) + params_delta(6);
|
||||
|
||||
% for rotation however, we want to make sure that the rotation matrix
|
||||
% approximation we have
|
||||
% R' = [1, -wz, wy
|
||||
% wz, 1, -wx
|
||||
% -wy, wx, 1]
|
||||
% is a legal rotation matrix, and then we combine it with current
|
||||
% rotation (through matrix multiplication) to acquire the new rotation
|
||||
|
||||
R = Euler2Rot(current_global(2:4));
|
||||
|
||||
wx = params_delta(2);
|
||||
wy = params_delta(3);
|
||||
wz = params_delta(4);
|
||||
|
||||
R_delta = [1, -wz, wy;
|
||||
wz, 1, -wx;
|
||||
-wy, wx, 1];
|
||||
|
||||
% Make sure R_delta is orthonormal
|
||||
R_delta = OrthonormaliseRotation(R_delta);
|
||||
|
||||
% Combine rotations
|
||||
R_final = R * R_delta;
|
||||
|
||||
% Extract euler angle
|
||||
euler = Rot2Euler(R_final);
|
||||
|
||||
rigid(2:4) = euler;
|
||||
|
||||
if(length(params_delta) > 6)
|
||||
% non-rigid parameters can just be added together
|
||||
non_rigid = params_delta(7:end) + current_non_rigid;
|
||||
else
|
||||
non_rigid = current_non_rigid;
|
||||
end
|
||||
|
||||
end
|
||||
|
||||
function R_ortho = OrthonormaliseRotation(R)
|
||||
|
||||
% U * V' is basically what we want, as it's guaranteed to be
|
||||
% orthonormal
|
||||
[U, ~, V] = svd(R);
|
||||
|
||||
% We also want to make sure no reflection happened
|
||||
|
||||
% get the orthogonal matrix from the initial rotation matrix
|
||||
X = U*V';
|
||||
|
||||
% This makes sure that the handedness is preserved and no reflection happened
|
||||
% by making sure the determinant is 1 and not -1
|
||||
W = eye(3);
|
||||
W(3,3) = det(X);
|
||||
R_ortho = U*W*V';
|
||||
end
|
||||
@@ -0,0 +1,340 @@
|
||||
function [ a, R, T, T3D, params, error, shapeOrtho ] = fit_PDM_ortho_proj_to_2D_no_reg( M, E, V, shape2D)
|
||||
%FITPDMTO2DSHAPE Summary of this function goes here
|
||||
% Detailed explanation goes here
|
||||
|
||||
hidden = false;
|
||||
|
||||
% if some of the points are unavailable modify M, V, and shape2D (can
|
||||
% later infer the actual shape from this)
|
||||
if(sum(shape2D(:)==0) > 0)
|
||||
|
||||
hidden = true;
|
||||
% which indices to remove
|
||||
inds_to_rem = shape2D(:,1) == 0 | shape2D(:,2) == 0;
|
||||
|
||||
shape2D = shape2D(~inds_to_rem,:);
|
||||
|
||||
inds_to_rem = repmat(inds_to_rem, 3, 1);
|
||||
|
||||
M_old = M;
|
||||
V_old = V;
|
||||
|
||||
M = M(~inds_to_rem);
|
||||
V = V(~inds_to_rem,:);
|
||||
|
||||
end
|
||||
|
||||
num_points = numel(M) / 3;
|
||||
|
||||
m = reshape(M, num_points, 3)';
|
||||
width_model = max(m(1,:)) - min(m(1,:));
|
||||
height_model = max(m(2,:)) - min(m(2,:));
|
||||
|
||||
bounding_box = [min(shape2D(:,1)), min(shape2D(:,2)),...
|
||||
max(shape2D(:,1)), max(shape2D(:,2))];
|
||||
|
||||
a = (((bounding_box(3) - bounding_box(1)) / width_model) + ((bounding_box(4) - bounding_box(2))/ height_model)) / 2;
|
||||
|
||||
tx = (bounding_box(3) + bounding_box(1))/2;
|
||||
ty = (bounding_box(4) + bounding_box(2))/2;
|
||||
|
||||
% correct it so that the bounding box is just around the minimum
|
||||
% and maximum point in the initialised face
|
||||
tx = tx - a*(min(m(1,:)) + max(m(1,:)))/2;
|
||||
ty = ty - a*(min(m(2,:)) + max(m(2,:)))/2;
|
||||
|
||||
R = eye(3);
|
||||
T = [tx; ty];
|
||||
|
||||
params = zeros(size(E));
|
||||
|
||||
currShape = getShapeOrtho(M, V, params, R, T, a);
|
||||
|
||||
currError = getRMSerror(currShape, shape2D);
|
||||
|
||||
reg_rigid = zeros(6,1);
|
||||
regFactor = 0.25;
|
||||
regularisations = [reg_rigid; regFactor ./ E]; % the above version, however, does not perform as well
|
||||
regularisations = diag(regularisations)*diag(regularisations);
|
||||
|
||||
red_in_a_row = 0;
|
||||
|
||||
for i=1:1000
|
||||
|
||||
shape3D = M + V * params;
|
||||
shape3D = reshape(shape3D, numel(shape3D) / 3, 3);
|
||||
|
||||
% Now find the current residual error
|
||||
currShape = a * R(1:2,:)*shape3D' + repmat(T, 1, numel(M)/3);
|
||||
currShape = currShape';
|
||||
|
||||
error_res = shape2D - currShape;
|
||||
|
||||
eul = Rot2Euler(R);
|
||||
|
||||
p_global = [a; eul'; T];
|
||||
|
||||
% get the Jacobians
|
||||
J = CalcJacobian(M, V, params, p_global);
|
||||
|
||||
% RLMS style update
|
||||
p_delta = (J'*J + regularisations) \ (J'*error_res(:) - regularisations*[p_global;params]);
|
||||
|
||||
% not to overshoot
|
||||
p_delta = 0.5 * p_delta;
|
||||
|
||||
[params, p_global] = CalcReferenceUpdate(p_delta, params, p_global);
|
||||
|
||||
a = p_global(1);
|
||||
R = Euler2Rot(p_global(2:4));
|
||||
T = p_global(5:6);
|
||||
|
||||
shape3D = M + V * params;
|
||||
shape3D = reshape(shape3D, numel(shape3D) / 3, 3);
|
||||
currShape = a * R(1:2,:)*shape3D' + repmat(T, 1, numel(M)/3);
|
||||
currShape = currShape';
|
||||
|
||||
error = getRMSerror(currShape, shape2D);
|
||||
|
||||
if(0.999 * currError < error)
|
||||
red_in_a_row = red_in_a_row + 1;
|
||||
if(red_in_a_row == 5)
|
||||
break;
|
||||
end
|
||||
end
|
||||
|
||||
currError = error;
|
||||
|
||||
end
|
||||
|
||||
if(hidden)
|
||||
shapeOrtho = getShapeOrtho(M_old, V_old, params, R, T, a);
|
||||
else
|
||||
shapeOrtho = currShape;
|
||||
end
|
||||
|
||||
T3D = [0;0;0];
|
||||
|
||||
end
|
||||
|
||||
function [shape2D] = getShapeOrtho(M, V, p, R, T, a)
|
||||
|
||||
% M - mean shape vector
|
||||
% V - eigenvectors
|
||||
% p - parameters of non-rigid shape
|
||||
% R - rotation matrix
|
||||
% T - translation vector (tx, ty)
|
||||
shape3D = getShape3D(M, V, p);
|
||||
shape2D = a * R(1:2,:)*shape3D' + repmat(T, 1, numel(M)/3);
|
||||
shape2D = shape2D';
|
||||
end
|
||||
|
||||
function [shape2D] = getShapeOrthoFull(M, V, p, R, T, a)
|
||||
|
||||
% M - mean shape vector
|
||||
% V - eigenvectors
|
||||
% p - parameters of non-rigid shape
|
||||
% R - rotation matrix
|
||||
% T - translation vector (tx, ty)
|
||||
T = [T; 0];
|
||||
shape3D = getShape3D(M, V, p);
|
||||
shape2D = a * R*shape3D' + repmat(T, 1, numel(M)/3);
|
||||
shape2D = shape2D';
|
||||
end
|
||||
|
||||
function [shape3D] = getShape3D(M, V, params)
|
||||
|
||||
shape3D = M + V * params;
|
||||
shape3D = reshape(shape3D, numel(shape3D) / 3, 3);
|
||||
|
||||
end
|
||||
|
||||
function [error] = getRMSerror(shape2Dv1, shape2Dv2)
|
||||
|
||||
error = sqrt(mean(reshape(shape2Dv1 - shape2Dv2, numel(shape2Dv1), 1).^2));
|
||||
|
||||
end
|
||||
|
||||
% This calculates the combined rigid with non-rigid Jacobian
|
||||
function J = CalcJacobian(M, V, p, p_global)
|
||||
|
||||
n = size(M, 1)/3;
|
||||
|
||||
non_rigid_modes = size(V,2);
|
||||
|
||||
J = zeros(n*2, 6 + non_rigid_modes);
|
||||
|
||||
|
||||
% now the layour is
|
||||
% ---------- Rigid part -------------------|----Non rigid part--------|
|
||||
% dx_1/ds, dx_1/dr1, ... dx_1/dtx, dx_1/dty dx_1/dp_1 ... dx_1/dp_m
|
||||
% dx_2/ds, dx_2/dr1, ... dx_2/dtx, dx_2/dty dx_2/dp_1 ... dx_2/dp_m
|
||||
% ...
|
||||
% dx_n/ds, dx_n/dr1, ... dx_n/dtx, dx_n/dty dx_n/dp_1 ... dx_n/dp_m
|
||||
% dy_1/ds, dy_1/dr1, ... dy_1/dtx, dy_1/dty dy_1/dp_1 ... dy_1/dp_m
|
||||
% ...
|
||||
% dy_n/ds, dy_n/dr1, ... dy_n/dtx, dy_n/dty dy_n/dp_1 ... dy_n/dp_m
|
||||
|
||||
% getting the rigid part
|
||||
J(:,1:6) = CalcRigidJacobian(M, V, p, p_global);
|
||||
|
||||
% constructing the non-rigid part
|
||||
R = Euler2Rot(p_global(2:4));
|
||||
s = p_global(1);
|
||||
|
||||
% 'rotate' and 'scale' the principal components
|
||||
|
||||
% First reshape to 3D
|
||||
V_X = V(1:n,:);
|
||||
V_Y = V(n+1:2*n,:);
|
||||
V_Z = V(2*n+1:end,:);
|
||||
|
||||
J_x_non_rigid = s*(R(1,1)*V_X + R(1,2)*V_Y + R(1,3)*V_Z);
|
||||
J_y_non_rigid = s*(R(2,1)*V_X + R(2,2)*V_Y + R(2,3)*V_Z);
|
||||
|
||||
J(1:n, 7:end) = J_x_non_rigid;
|
||||
J(n+1:end, 7:end) = J_y_non_rigid;
|
||||
|
||||
end
|
||||
|
||||
function J = CalcRigidJacobian(M, V, p, p_global)
|
||||
|
||||
n = size(M, 1)/3;
|
||||
|
||||
% Get the current 3D shape (not affected by global transform, as this
|
||||
% is how the Jacobian was derived (for derivation please see
|
||||
% ../derivations/orthoJacobian
|
||||
shape3D = GetShape3D(M, V, p);
|
||||
|
||||
% Get the rotation matrix corresponding to current global orientation
|
||||
R = Euler2Rot(p_global(2:4));
|
||||
s = p_global(1);
|
||||
|
||||
% Rigid Jacobian is laid out as follows
|
||||
% dx_1/ds, dx_1/dr1, dx_1/dr2, dx_1/dr3, dx_1/dtx, dx_1/dty
|
||||
% dx_2/ds, dx_2/dr1, dx_2/dr2, dx_2/dr3, dx_2/dtx, dx_2/dty
|
||||
% ...
|
||||
% dx_n/ds, dx_n/dr1, dx_n/dr2, dx_n/dr3, dx_n/dtx, dx_n/dty
|
||||
% dy_1/ds, dy_1/dr1, dy_1/dr2, dy_1/dr3, dy_1/dtx, dy_1/dty
|
||||
% ...
|
||||
% dy_n/ds, dy_n/dr1, dy_n/dr2, dy_n/dr3, dy_n/dtx, dy_n/dty
|
||||
|
||||
J = zeros(n*2, 6);
|
||||
|
||||
% dx/ds = X * r11 + Y * r12 + Z * r13
|
||||
% dx/dr1 = s*(r13 * Y - r12 * Z)
|
||||
% dx/dr2 = -s*(r13 * X - r11 * Z)
|
||||
% dx/dr3 = s*(r12 * X - r11 * Y)
|
||||
% dx/dtx = 1
|
||||
% dx/dty = 0
|
||||
|
||||
% dy/ds = X * r21 + Y * r22 + Z * r23
|
||||
% dy/dr1 = s * (r23 * Y - r22 * Z)
|
||||
% dy/dr2 = -s * (r23 * X - r21 * Z)
|
||||
% dy/dr3 = s * (r22 * X - r21 * Y)
|
||||
% dy/dtx = 0
|
||||
% dy/dty = 1
|
||||
|
||||
% set the Jacobian for x's
|
||||
|
||||
% with respect to scaling factor
|
||||
J(1:n,1) = shape3D * R(1,:)';
|
||||
|
||||
% with respect to angular rotation around x, y, and z axes
|
||||
|
||||
% Change of x with respect to change in axis angle rotation
|
||||
dxdR = [ 0, R(1,3), -R(1,2);
|
||||
-R(1,3), 0, R(1,1);
|
||||
R(1,2), -R(1,1), 0];
|
||||
|
||||
J(1:n,2:4) = s*(dxdR * shape3D')';
|
||||
|
||||
% with respect to translation
|
||||
J(1:n,5) = 1;
|
||||
J(1:n,6) = 0;
|
||||
|
||||
% set the Jacobian for y's
|
||||
|
||||
% with respect to scaling factor
|
||||
J(n+1:end,1) = shape3D * R(2,:)';
|
||||
|
||||
% with respect to angular rotation around x, y, and z axes
|
||||
|
||||
% Change of y with respect to change in axis angle rotation
|
||||
dydR = [ 0, R(2,3), -R(2,2);
|
||||
-R(2,3), 0, R(2,1);
|
||||
R(2,2), -R(2,1), 0];
|
||||
|
||||
J(n+1:end,2:4) = s*(dydR * shape3D')';
|
||||
|
||||
% with respect to translation
|
||||
J(n+1:end,5) = 0;
|
||||
J(n+1:end,6) = 1;
|
||||
|
||||
end
|
||||
|
||||
% This updates the parameters based on the updates from the RLMS
|
||||
function [non_rigid, rigid] = CalcReferenceUpdate(params_delta, current_non_rigid, current_global)
|
||||
|
||||
|
||||
rigid = zeros(6, 1);
|
||||
% Same goes for scaling and translation parameters
|
||||
rigid(1) = current_global(1) + params_delta(1);
|
||||
rigid(5) = current_global(5) + params_delta(5);
|
||||
rigid(6) = current_global(6) + params_delta(6);
|
||||
|
||||
% for rotation however, we want to make sure that the rotation matrix
|
||||
% approximation we have
|
||||
% R' = [1, -wz, wy
|
||||
% wz, 1, -wx
|
||||
% -wy, wx, 1]
|
||||
% is a legal rotation matrix, and then we combine it with current
|
||||
% rotation (through matrix multiplication) to acquire the new rotation
|
||||
|
||||
R = Euler2Rot(current_global(2:4));
|
||||
|
||||
wx = params_delta(2);
|
||||
wy = params_delta(3);
|
||||
wz = params_delta(4);
|
||||
|
||||
R_delta = [1, -wz, wy;
|
||||
wz, 1, -wx;
|
||||
-wy, wx, 1];
|
||||
|
||||
% Make sure R_delta is orthonormal
|
||||
R_delta = OrthonormaliseRotation(R_delta);
|
||||
|
||||
% Combine rotations
|
||||
R_final = R * R_delta;
|
||||
|
||||
% Extract euler angle
|
||||
euler = Rot2Euler(R_final);
|
||||
|
||||
rigid(2:4) = euler;
|
||||
|
||||
if(length(params_delta) > 6)
|
||||
% non-rigid parameters can just be added together
|
||||
non_rigid = params_delta(7:end) + current_non_rigid;
|
||||
else
|
||||
non_rigid = current_non_rigid;
|
||||
end
|
||||
|
||||
end
|
||||
|
||||
function R_ortho = OrthonormaliseRotation(R)
|
||||
|
||||
% U * V' is basically what we want, as it's guaranteed to be
|
||||
% orthonormal
|
||||
[U, ~, V] = svd(R);
|
||||
|
||||
% We also want to make sure no reflection happened
|
||||
|
||||
% get the orthogonal matrix from the initial rotation matrix
|
||||
X = U*V';
|
||||
|
||||
% This makes sure that the handedness is preserved and no reflection happened
|
||||
% by making sure the determinant is 1 and not -1
|
||||
W = eye(3);
|
||||
W(3,3) = det(X);
|
||||
R_ortho = U*W*V';
|
||||
end
|
||||
32
pkg/OpenFace/matlab_version/PDM_helpers/iterate_piece_wise.m
Normal file
32
pkg/OpenFace/matlab_version/PDM_helpers/iterate_piece_wise.m
Normal file
@@ -0,0 +1,32 @@
|
||||
function [ pts_new ] = iterate_piece_wise( pts_orig, new_num_points )
|
||||
%ITERATE_PIECE_WISE Summary of this function goes here
|
||||
% Detailed explanation goes here
|
||||
|
||||
% Reinterpolate the new points, but make sure they are still on the
|
||||
% same lines
|
||||
num_orig = size(pts_orig,1);
|
||||
|
||||
% Divide the number of original segments by number of new segments
|
||||
step_size = (num_orig - 1) / (new_num_points-1);
|
||||
|
||||
pts_new = zeros(new_num_points,2);
|
||||
|
||||
% Clamp the beginning and end, as they will be the same
|
||||
pts_new(1,:) = pts_orig(1,:);
|
||||
pts_new(end,:) = pts_orig(end,:);
|
||||
|
||||
for i=1:new_num_points-2
|
||||
|
||||
low_point = floor(1 + i * step_size);
|
||||
high_point = ceil(1 + i * step_size);
|
||||
|
||||
coeff_1 = floor(1 + i * step_size) - i * step_size;
|
||||
coeff_2 = 1 - coeff_1;
|
||||
|
||||
new_pt = coeff_1 * pts_orig(low_point,:) + coeff_2 * pts_orig(high_point,:);
|
||||
pts_new(i+1,:) = new_pt;
|
||||
|
||||
end
|
||||
|
||||
end
|
||||
|
||||
16
pkg/OpenFace/matlab_version/PDM_helpers/writeMatrix.m
Normal file
16
pkg/OpenFace/matlab_version/PDM_helpers/writeMatrix.m
Normal file
@@ -0,0 +1,16 @@
|
||||
% for easier readibility write them row by row
|
||||
function writeMatrix(fileID, M, type)
|
||||
|
||||
fprintf(fileID, '%d\r\n', size(M,1));
|
||||
fprintf(fileID, '%d\r\n', size(M,2));
|
||||
fprintf(fileID, '%d\r\n', type);
|
||||
|
||||
for i=1:size(M,1)
|
||||
if(type == 4 || type == 0)
|
||||
fprintf(fileID, '%d ', M(i,:));
|
||||
else
|
||||
fprintf(fileID, '%.9f ', M(i,:));
|
||||
end
|
||||
fprintf(fileID, '\r\n');
|
||||
end
|
||||
end
|
||||
37
pkg/OpenFace/matlab_version/PDM_helpers/writeMatrixBin.m
Normal file
37
pkg/OpenFace/matlab_version/PDM_helpers/writeMatrixBin.m
Normal file
@@ -0,0 +1,37 @@
|
||||
% for easier readibility write them row by row
|
||||
function writeMatrixBin(fileID, M, type)
|
||||
|
||||
% 4 bytes each for the description
|
||||
fwrite(fileID, size(M,1), 'uint');
|
||||
fwrite(fileID, size(M,2), 'uint');
|
||||
fwrite(fileID, type, 'uint');
|
||||
|
||||
% Convert the matrix to OpenCV format (row minor as opposed to column
|
||||
% minor)
|
||||
M = M';
|
||||
|
||||
% type 0 - uint8, 1 - int8, 2 - uint16, 3 - int16, 4 - int, 5 -
|
||||
% float32, 6 - float64
|
||||
|
||||
% Write out the matrix itself
|
||||
|
||||
switch type
|
||||
case 0
|
||||
type = 'uint8';
|
||||
case 1
|
||||
type = 'int8';
|
||||
case 2
|
||||
type = 'uint16';
|
||||
case 3
|
||||
type = 'int16';
|
||||
case 4
|
||||
type = 'int';
|
||||
case 5
|
||||
type = 'float32';
|
||||
case 6
|
||||
type = 'float64';
|
||||
otherwise
|
||||
type = 'float32';
|
||||
end
|
||||
fwrite(fileID, M, type);
|
||||
end
|
||||
Reference in New Issue
Block a user