2014-02-10 02:10:30 +01:00
|
|
|
/*************************************************************************/
|
|
|
|
/* matrix3.cpp */
|
|
|
|
/*************************************************************************/
|
|
|
|
/* This file is part of: */
|
|
|
|
/* GODOT ENGINE */
|
|
|
|
/* http://www.godotengine.org */
|
|
|
|
/*************************************************************************/
|
2017-01-01 22:01:57 +01:00
|
|
|
/* Copyright (c) 2007-2017 Juan Linietsky, Ariel Manzur. */
|
2014-02-10 02:10:30 +01:00
|
|
|
/* */
|
|
|
|
/* Permission is hereby granted, free of charge, to any person obtaining */
|
|
|
|
/* a copy of this software and associated documentation files (the */
|
|
|
|
/* "Software"), to deal in the Software without restriction, including */
|
|
|
|
/* without limitation the rights to use, copy, modify, merge, publish, */
|
|
|
|
/* distribute, sublicense, and/or sell copies of the Software, and to */
|
|
|
|
/* permit persons to whom the Software is furnished to do so, subject to */
|
|
|
|
/* the following conditions: */
|
|
|
|
/* */
|
|
|
|
/* The above copyright notice and this permission notice shall be */
|
|
|
|
/* included in all copies or substantial portions of the Software. */
|
|
|
|
/* */
|
|
|
|
/* THE SOFTWARE IS PROVIDED "AS IS", WITHOUT WARRANTY OF ANY KIND, */
|
|
|
|
/* EXPRESS OR IMPLIED, INCLUDING BUT NOT LIMITED TO THE WARRANTIES OF */
|
|
|
|
/* MERCHANTABILITY, FITNESS FOR A PARTICULAR PURPOSE AND NONINFRINGEMENT.*/
|
|
|
|
/* IN NO EVENT SHALL THE AUTHORS OR COPYRIGHT HOLDERS BE LIABLE FOR ANY */
|
|
|
|
/* CLAIM, DAMAGES OR OTHER LIABILITY, WHETHER IN AN ACTION OF CONTRACT, */
|
|
|
|
/* TORT OR OTHERWISE, ARISING FROM, OUT OF OR IN CONNECTION WITH THE */
|
|
|
|
/* SOFTWARE OR THE USE OR OTHER DEALINGS IN THE SOFTWARE. */
|
|
|
|
/*************************************************************************/
|
|
|
|
#include "matrix3.h"
|
|
|
|
#include "math_funcs.h"
|
|
|
|
#include "os/copymem.h"
|
|
|
|
|
|
|
|
#define cofac(row1,col1, row2, col2)\
|
|
|
|
(elements[row1][col1] * elements[row2][col2] - elements[row1][col2] * elements[row2][col1])
|
|
|
|
|
|
|
|
void Matrix3::from_z(const Vector3& p_z) {
|
|
|
|
|
|
|
|
if (Math::abs(p_z.z) > Math_SQRT12 ) {
|
|
|
|
|
|
|
|
// choose p in y-z plane
|
|
|
|
real_t a = p_z[1]*p_z[1] + p_z[2]*p_z[2];
|
|
|
|
real_t k = 1.0/Math::sqrt(a);
|
|
|
|
elements[0]=Vector3(0,-p_z[2]*k,p_z[1]*k);
|
|
|
|
elements[1]=Vector3(a*k,-p_z[0]*elements[0][2],p_z[0]*elements[0][1]);
|
|
|
|
} else {
|
|
|
|
|
|
|
|
// choose p in x-y plane
|
|
|
|
real_t a = p_z.x*p_z.x + p_z.y*p_z.y;
|
|
|
|
real_t k = 1.0/Math::sqrt(a);
|
|
|
|
elements[0]=Vector3(-p_z.y*k,p_z.x*k,0);
|
|
|
|
elements[1]=Vector3(-p_z.z*elements[0].y,p_z.z*elements[0].x,a*k);
|
|
|
|
}
|
|
|
|
elements[2]=p_z;
|
|
|
|
}
|
|
|
|
|
|
|
|
void Matrix3::invert() {
|
|
|
|
|
|
|
|
|
|
|
|
real_t co[3]={
|
|
|
|
cofac(1, 1, 2, 2), cofac(1, 2, 2, 0), cofac(1, 0, 2, 1)
|
|
|
|
};
|
|
|
|
real_t det = elements[0][0] * co[0]+
|
|
|
|
elements[0][1] * co[1]+
|
|
|
|
elements[0][2] * co[2];
|
2016-03-09 00:00:52 +01:00
|
|
|
|
2014-02-10 02:10:30 +01:00
|
|
|
ERR_FAIL_COND( det == 0 );
|
|
|
|
real_t s = 1.0/det;
|
2016-03-09 00:00:52 +01:00
|
|
|
|
|
|
|
set( co[0]*s, cofac(0, 2, 2, 1) * s, cofac(0, 1, 1, 2) * s,
|
2014-02-10 02:10:30 +01:00
|
|
|
co[1]*s, cofac(0, 0, 2, 2) * s, cofac(0, 2, 1, 0) * s,
|
|
|
|
co[2]*s, cofac(0, 1, 2, 0) * s, cofac(0, 0, 1, 1) * s );
|
|
|
|
|
|
|
|
}
|
|
|
|
|
|
|
|
void Matrix3::orthonormalize() {
|
2016-10-18 22:50:21 +02:00
|
|
|
ERR_FAIL_COND(determinant() == 0);
|
2014-02-10 02:10:30 +01:00
|
|
|
|
|
|
|
// Gram-Schmidt Process
|
|
|
|
|
|
|
|
Vector3 x=get_axis(0);
|
|
|
|
Vector3 y=get_axis(1);
|
|
|
|
Vector3 z=get_axis(2);
|
|
|
|
|
|
|
|
x.normalize();
|
|
|
|
y = (y-x*(x.dot(y)));
|
|
|
|
y.normalize();
|
|
|
|
z = (z-x*(x.dot(z))-y*(y.dot(z)));
|
|
|
|
z.normalize();
|
|
|
|
|
|
|
|
set_axis(0,x);
|
|
|
|
set_axis(1,y);
|
|
|
|
set_axis(2,z);
|
|
|
|
|
|
|
|
}
|
|
|
|
|
|
|
|
Matrix3 Matrix3::orthonormalized() const {
|
|
|
|
|
|
|
|
Matrix3 c = *this;
|
|
|
|
c.orthonormalize();
|
|
|
|
return c;
|
|
|
|
}
|
|
|
|
|
2016-10-18 22:50:21 +02:00
|
|
|
bool Matrix3::is_orthogonal() const {
|
|
|
|
Matrix3 id;
|
|
|
|
Matrix3 m = (*this)*transposed();
|
|
|
|
|
|
|
|
return isequal_approx(id,m);
|
|
|
|
}
|
|
|
|
|
|
|
|
bool Matrix3::is_rotation() const {
|
|
|
|
return Math::isequal_approx(determinant(), 1) && is_orthogonal();
|
|
|
|
}
|
|
|
|
|
2014-02-10 02:10:30 +01:00
|
|
|
|
|
|
|
Matrix3 Matrix3::inverse() const {
|
|
|
|
|
|
|
|
Matrix3 inv=*this;
|
|
|
|
inv.invert();
|
|
|
|
return inv;
|
|
|
|
}
|
|
|
|
|
|
|
|
void Matrix3::transpose() {
|
|
|
|
|
|
|
|
SWAP(elements[0][1],elements[1][0]);
|
|
|
|
SWAP(elements[0][2],elements[2][0]);
|
|
|
|
SWAP(elements[1][2],elements[2][1]);
|
|
|
|
}
|
|
|
|
|
|
|
|
Matrix3 Matrix3::transposed() const {
|
|
|
|
|
|
|
|
Matrix3 tr=*this;
|
|
|
|
tr.transpose();
|
|
|
|
return tr;
|
|
|
|
}
|
|
|
|
|
|
|
|
void Matrix3::scale(const Vector3& p_scale) {
|
|
|
|
|
|
|
|
elements[0][0]*=p_scale.x;
|
|
|
|
elements[1][0]*=p_scale.x;
|
|
|
|
elements[2][0]*=p_scale.x;
|
|
|
|
elements[0][1]*=p_scale.y;
|
|
|
|
elements[1][1]*=p_scale.y;
|
|
|
|
elements[2][1]*=p_scale.y;
|
|
|
|
elements[0][2]*=p_scale.z;
|
|
|
|
elements[1][2]*=p_scale.z;
|
|
|
|
elements[2][2]*=p_scale.z;
|
|
|
|
}
|
|
|
|
|
|
|
|
Matrix3 Matrix3::scaled( const Vector3& p_scale ) const {
|
|
|
|
|
|
|
|
Matrix3 m = *this;
|
|
|
|
m.scale(p_scale);
|
|
|
|
return m;
|
|
|
|
}
|
|
|
|
|
|
|
|
Vector3 Matrix3::get_scale() const {
|
|
|
|
|
|
|
|
return Vector3(
|
|
|
|
Vector3(elements[0][0],elements[1][0],elements[2][0]).length(),
|
|
|
|
Vector3(elements[0][1],elements[1][1],elements[2][1]).length(),
|
|
|
|
Vector3(elements[0][2],elements[1][2],elements[2][2]).length()
|
|
|
|
);
|
2016-03-09 00:00:52 +01:00
|
|
|
|
2014-02-10 02:10:30 +01:00
|
|
|
}
|
|
|
|
|
2016-10-18 22:50:21 +02:00
|
|
|
// Matrix3::rotate and Matrix3::rotated return M * R(axis,phi), and is a convenience function. They do *not* perform proper matrix rotation.
|
|
|
|
void Matrix3::rotate(const Vector3& p_axis, real_t p_phi) {
|
|
|
|
// TODO: This function should also be renamed as the current name is misleading: rotate does *not* perform matrix rotation.
|
|
|
|
// Same problem affects Matrix3::rotated.
|
|
|
|
// A similar problem exists in 2D math, which will be handled separately.
|
|
|
|
// After Matrix3 is renamed to Basis, this comments needs to be revised.
|
2014-02-10 02:10:30 +01:00
|
|
|
*this = *this * Matrix3(p_axis, p_phi);
|
|
|
|
}
|
|
|
|
|
|
|
|
Matrix3 Matrix3::rotated(const Vector3& p_axis, real_t p_phi) const {
|
|
|
|
return *this * Matrix3(p_axis, p_phi);
|
|
|
|
|
|
|
|
}
|
|
|
|
|
2016-10-18 22:50:21 +02:00
|
|
|
// get_euler returns a vector containing the Euler angles in the format
|
|
|
|
// (a1,a2,a3), where a3 is the angle of the first rotation, and a1 is the last
|
|
|
|
// (following the convention they are commonly defined in the literature).
|
|
|
|
//
|
|
|
|
// The current implementation uses XYZ convention (Z is the first rotation),
|
|
|
|
// so euler.z is the angle of the (first) rotation around Z axis and so on,
|
|
|
|
//
|
|
|
|
// And thus, assuming the matrix is a rotation matrix, this function returns
|
|
|
|
// the angles in the decomposition R = X(a1).Y(a2).Z(a3) where Z(a) rotates
|
|
|
|
// around the z-axis by a and so on.
|
2014-02-10 02:10:30 +01:00
|
|
|
Vector3 Matrix3::get_euler() const {
|
|
|
|
|
2016-10-18 22:50:21 +02:00
|
|
|
// Euler angles in XYZ convention.
|
|
|
|
// See https://en.wikipedia.org/wiki/Euler_angles#Rotation_matrix
|
|
|
|
//
|
2014-02-10 02:10:30 +01:00
|
|
|
// rot = cy*cz -cy*sz sy
|
2016-10-18 22:50:21 +02:00
|
|
|
// cz*sx*sy+cx*sz cx*cz-sx*sy*sz -cy*sx
|
|
|
|
// -cx*cz*sy+sx*sz cz*sx+cx*sy*sz cx*cy
|
2014-02-10 02:10:30 +01:00
|
|
|
|
|
|
|
Vector3 euler;
|
|
|
|
|
2016-10-18 22:50:21 +02:00
|
|
|
ERR_FAIL_COND_V(is_rotation() == false, euler);
|
|
|
|
|
|
|
|
euler.y = Math::asin(elements[0][2]);
|
2014-02-10 02:10:30 +01:00
|
|
|
if ( euler.y < Math_PI*0.5) {
|
|
|
|
if ( euler.y > -Math_PI*0.5) {
|
2016-10-18 22:50:21 +02:00
|
|
|
euler.x = Math::atan2(-elements[1][2],elements[2][2]);
|
|
|
|
euler.z = Math::atan2(-elements[0][1],elements[0][0]);
|
2014-02-10 02:10:30 +01:00
|
|
|
|
|
|
|
} else {
|
2016-10-18 22:50:21 +02:00
|
|
|
real_t r = Math::atan2(elements[1][0],elements[1][1]);
|
2014-02-10 02:10:30 +01:00
|
|
|
euler.z = 0.0;
|
|
|
|
euler.x = euler.z - r;
|
|
|
|
|
|
|
|
}
|
|
|
|
} else {
|
2016-10-18 22:50:21 +02:00
|
|
|
real_t r = Math::atan2(elements[0][1],elements[1][1]);
|
2014-02-10 02:10:30 +01:00
|
|
|
euler.z = 0;
|
|
|
|
euler.x = r - euler.z;
|
|
|
|
}
|
|
|
|
|
|
|
|
return euler;
|
|
|
|
|
|
|
|
|
|
|
|
}
|
|
|
|
|
2016-10-18 22:50:21 +02:00
|
|
|
// set_euler expects a vector containing the Euler angles in the format
|
|
|
|
// (c,b,a), where a is the angle of the first rotation, and c is the last.
|
|
|
|
// The current implementation uses XYZ convention (Z is the first rotation).
|
2014-02-10 02:10:30 +01:00
|
|
|
void Matrix3::set_euler(const Vector3& p_euler) {
|
|
|
|
|
|
|
|
real_t c, s;
|
|
|
|
|
|
|
|
c = Math::cos(p_euler.x);
|
|
|
|
s = Math::sin(p_euler.x);
|
|
|
|
Matrix3 xmat(1.0,0.0,0.0,0.0,c,-s,0.0,s,c);
|
|
|
|
|
|
|
|
c = Math::cos(p_euler.y);
|
|
|
|
s = Math::sin(p_euler.y);
|
|
|
|
Matrix3 ymat(c,0.0,s,0.0,1.0,0.0,-s,0.0,c);
|
|
|
|
|
|
|
|
c = Math::cos(p_euler.z);
|
|
|
|
s = Math::sin(p_euler.z);
|
|
|
|
Matrix3 zmat(c,-s,0.0,s,c,0.0,0.0,0.0,1.0);
|
|
|
|
|
|
|
|
//optimizer will optimize away all this anyway
|
|
|
|
*this = xmat*(ymat*zmat);
|
|
|
|
}
|
|
|
|
|
2016-10-18 22:50:21 +02:00
|
|
|
bool Matrix3::isequal_approx(const Matrix3& a, const Matrix3& b) const {
|
|
|
|
|
|
|
|
for (int i=0;i<3;i++) {
|
|
|
|
for (int j=0;j<3;j++) {
|
|
|
|
if (Math::isequal_approx(a.elements[i][j],b.elements[i][j]) == false)
|
|
|
|
return false;
|
|
|
|
}
|
|
|
|
}
|
|
|
|
|
|
|
|
return true;
|
|
|
|
}
|
|
|
|
|
2014-02-10 02:10:30 +01:00
|
|
|
bool Matrix3::operator==(const Matrix3& p_matrix) const {
|
|
|
|
|
|
|
|
for (int i=0;i<3;i++) {
|
|
|
|
for (int j=0;j<3;j++) {
|
2016-10-18 22:50:21 +02:00
|
|
|
if (elements[i][j] != p_matrix.elements[i][j])
|
2014-02-10 02:10:30 +01:00
|
|
|
return false;
|
|
|
|
}
|
|
|
|
}
|
2016-03-09 00:00:52 +01:00
|
|
|
|
2014-02-10 02:10:30 +01:00
|
|
|
return true;
|
|
|
|
}
|
2016-10-18 22:50:21 +02:00
|
|
|
|
2014-02-10 02:10:30 +01:00
|
|
|
bool Matrix3::operator!=(const Matrix3& p_matrix) const {
|
|
|
|
|
|
|
|
return (!(*this==p_matrix));
|
|
|
|
}
|
|
|
|
|
|
|
|
Matrix3::operator String() const {
|
|
|
|
|
|
|
|
String mtx;
|
|
|
|
for (int i=0;i<3;i++) {
|
2016-03-09 00:00:52 +01:00
|
|
|
|
2014-02-10 02:10:30 +01:00
|
|
|
for (int j=0;j<3;j++) {
|
2016-03-09 00:00:52 +01:00
|
|
|
|
2014-02-10 02:10:30 +01:00
|
|
|
if (i!=0 || j!=0)
|
|
|
|
mtx+=", ";
|
2016-03-09 00:00:52 +01:00
|
|
|
|
2014-02-10 02:10:30 +01:00
|
|
|
mtx+=rtos( elements[i][j] );
|
|
|
|
}
|
|
|
|
}
|
2016-03-09 00:00:52 +01:00
|
|
|
|
2014-02-10 02:10:30 +01:00
|
|
|
return mtx;
|
|
|
|
}
|
|
|
|
|
|
|
|
Matrix3::operator Quat() const {
|
2016-10-18 22:50:21 +02:00
|
|
|
ERR_FAIL_COND_V(is_rotation() == false, Quat());
|
2014-02-10 02:10:30 +01:00
|
|
|
|
2016-10-18 22:50:21 +02:00
|
|
|
real_t trace = elements[0][0] + elements[1][1] + elements[2][2];
|
2014-02-10 02:10:30 +01:00
|
|
|
real_t temp[4];
|
2016-03-09 00:00:52 +01:00
|
|
|
|
|
|
|
if (trace > 0.0)
|
2014-02-10 02:10:30 +01:00
|
|
|
{
|
|
|
|
real_t s = Math::sqrt(trace + 1.0);
|
|
|
|
temp[3]=(s * 0.5);
|
|
|
|
s = 0.5 / s;
|
2016-03-09 00:00:52 +01:00
|
|
|
|
2016-10-18 22:50:21 +02:00
|
|
|
temp[0]=((elements[2][1] - elements[1][2]) * s);
|
|
|
|
temp[1]=((elements[0][2] - elements[2][0]) * s);
|
|
|
|
temp[2]=((elements[1][0] - elements[0][1]) * s);
|
2016-03-09 00:00:52 +01:00
|
|
|
}
|
|
|
|
else
|
2014-02-10 02:10:30 +01:00
|
|
|
{
|
2016-10-18 22:50:21 +02:00
|
|
|
int i = elements[0][0] < elements[1][1] ?
|
|
|
|
(elements[1][1] < elements[2][2] ? 2 : 1) :
|
|
|
|
(elements[0][0] < elements[2][2] ? 2 : 0);
|
2016-03-09 00:00:52 +01:00
|
|
|
int j = (i + 1) % 3;
|
2014-02-10 02:10:30 +01:00
|
|
|
int k = (i + 2) % 3;
|
2016-03-09 00:00:52 +01:00
|
|
|
|
2016-10-18 22:50:21 +02:00
|
|
|
real_t s = Math::sqrt(elements[i][i] - elements[j][j] - elements[k][k] + 1.0);
|
2014-02-10 02:10:30 +01:00
|
|
|
temp[i] = s * 0.5;
|
|
|
|
s = 0.5 / s;
|
2016-03-09 00:00:52 +01:00
|
|
|
|
2016-10-18 22:50:21 +02:00
|
|
|
temp[3] = (elements[k][j] - elements[j][k]) * s;
|
|
|
|
temp[j] = (elements[j][i] + elements[i][j]) * s;
|
|
|
|
temp[k] = (elements[k][i] + elements[i][k]) * s;
|
2014-02-10 02:10:30 +01:00
|
|
|
}
|
2016-03-09 00:00:52 +01:00
|
|
|
|
2014-02-10 02:10:30 +01:00
|
|
|
return Quat(temp[0],temp[1],temp[2],temp[3]);
|
|
|
|
|
|
|
|
}
|
|
|
|
|
|
|
|
static const Matrix3 _ortho_bases[24]={
|
|
|
|
Matrix3(1, 0, 0, 0, 1, 0, 0, 0, 1),
|
|
|
|
Matrix3(0, -1, 0, 1, 0, 0, 0, 0, 1),
|
|
|
|
Matrix3(-1, 0, 0, 0, -1, 0, 0, 0, 1),
|
|
|
|
Matrix3(0, 1, 0, -1, 0, 0, 0, 0, 1),
|
|
|
|
Matrix3(1, 0, 0, 0, 0, -1, 0, 1, 0),
|
|
|
|
Matrix3(0, 0, 1, 1, 0, 0, 0, 1, 0),
|
|
|
|
Matrix3(-1, 0, 0, 0, 0, 1, 0, 1, 0),
|
|
|
|
Matrix3(0, 0, -1, -1, 0, 0, 0, 1, 0),
|
|
|
|
Matrix3(1, 0, 0, 0, -1, 0, 0, 0, -1),
|
|
|
|
Matrix3(0, 1, 0, 1, 0, 0, 0, 0, -1),
|
|
|
|
Matrix3(-1, 0, 0, 0, 1, 0, 0, 0, -1),
|
|
|
|
Matrix3(0, -1, 0, -1, 0, 0, 0, 0, -1),
|
|
|
|
Matrix3(1, 0, 0, 0, 0, 1, 0, -1, 0),
|
|
|
|
Matrix3(0, 0, -1, 1, 0, 0, 0, -1, 0),
|
|
|
|
Matrix3(-1, 0, 0, 0, 0, -1, 0, -1, 0),
|
|
|
|
Matrix3(0, 0, 1, -1, 0, 0, 0, -1, 0),
|
|
|
|
Matrix3(0, 0, 1, 0, 1, 0, -1, 0, 0),
|
|
|
|
Matrix3(0, -1, 0, 0, 0, 1, -1, 0, 0),
|
|
|
|
Matrix3(0, 0, -1, 0, -1, 0, -1, 0, 0),
|
|
|
|
Matrix3(0, 1, 0, 0, 0, -1, -1, 0, 0),
|
|
|
|
Matrix3(0, 0, 1, 0, -1, 0, 1, 0, 0),
|
|
|
|
Matrix3(0, 1, 0, 0, 0, 1, 1, 0, 0),
|
|
|
|
Matrix3(0, 0, -1, 0, 1, 0, 1, 0, 0),
|
|
|
|
Matrix3(0, -1, 0, 0, 0, -1, 1, 0, 0)
|
|
|
|
};
|
|
|
|
|
|
|
|
int Matrix3::get_orthogonal_index() const {
|
|
|
|
|
|
|
|
//could be sped up if i come up with a way
|
|
|
|
Matrix3 orth=*this;
|
|
|
|
for(int i=0;i<3;i++) {
|
|
|
|
for(int j=0;j<3;j++) {
|
|
|
|
|
|
|
|
float v = orth[i][j];
|
|
|
|
if (v>0.5)
|
|
|
|
v=1.0;
|
|
|
|
else if (v<-0.5)
|
|
|
|
v=-1.0;
|
|
|
|
else
|
|
|
|
v=0;
|
|
|
|
|
|
|
|
orth[i][j]=v;
|
|
|
|
}
|
|
|
|
}
|
|
|
|
|
|
|
|
for(int i=0;i<24;i++) {
|
|
|
|
|
|
|
|
if (_ortho_bases[i]==orth)
|
|
|
|
return i;
|
|
|
|
|
|
|
|
|
|
|
|
}
|
|
|
|
|
|
|
|
return 0;
|
|
|
|
}
|
|
|
|
|
|
|
|
void Matrix3::set_orthogonal_index(int p_index){
|
|
|
|
|
|
|
|
//there only exist 24 orthogonal bases in r3
|
|
|
|
ERR_FAIL_INDEX(p_index,24);
|
|
|
|
|
|
|
|
|
|
|
|
*this=_ortho_bases[p_index];
|
|
|
|
|
|
|
|
}
|
|
|
|
|
|
|
|
|
|
|
|
void Matrix3::get_axis_and_angle(Vector3 &r_axis,real_t& r_angle) const {
|
2016-10-18 22:50:21 +02:00
|
|
|
// TODO: We can handle improper matrices here too, in which case axis will also correspond to the axis of reflection.
|
|
|
|
// See Eq. (52) in http://scipp.ucsc.edu/~haber/ph251/rotreflect_13.pdf for example
|
|
|
|
// After that change, we should fail on is_orthogonal() == false.
|
|
|
|
ERR_FAIL_COND(is_rotation() == false);
|
2014-02-10 02:10:30 +01:00
|
|
|
|
|
|
|
|
|
|
|
double angle,x,y,z; // variables for result
|
|
|
|
double epsilon = 0.01; // margin to allow for rounding errors
|
|
|
|
double epsilon2 = 0.1; // margin to distinguish between 0 and 180 degrees
|
|
|
|
|
|
|
|
if ( (Math::abs(elements[1][0]-elements[0][1])< epsilon)
|
|
|
|
&& (Math::abs(elements[2][0]-elements[0][2])< epsilon)
|
|
|
|
&& (Math::abs(elements[2][1]-elements[1][2])< epsilon)) {
|
|
|
|
// singularity found
|
|
|
|
// first check for identity matrix which must have +1 for all terms
|
|
|
|
// in leading diagonaland zero in other terms
|
|
|
|
if ((Math::abs(elements[1][0]+elements[0][1]) < epsilon2)
|
|
|
|
&& (Math::abs(elements[2][0]+elements[0][2]) < epsilon2)
|
|
|
|
&& (Math::abs(elements[2][1]+elements[1][2]) < epsilon2)
|
|
|
|
&& (Math::abs(elements[0][0]+elements[1][1]+elements[2][2]-3) < epsilon2)) {
|
|
|
|
// this singularity is identity matrix so angle = 0
|
|
|
|
r_axis=Vector3(0,1,0);
|
|
|
|
r_angle=0;
|
|
|
|
return;
|
|
|
|
}
|
|
|
|
// otherwise this singularity is angle = 180
|
|
|
|
angle = Math_PI;
|
|
|
|
double xx = (elements[0][0]+1)/2;
|
|
|
|
double yy = (elements[1][1]+1)/2;
|
|
|
|
double zz = (elements[2][2]+1)/2;
|
|
|
|
double xy = (elements[1][0]+elements[0][1])/4;
|
|
|
|
double xz = (elements[2][0]+elements[0][2])/4;
|
|
|
|
double yz = (elements[2][1]+elements[1][2])/4;
|
|
|
|
if ((xx > yy) && (xx > zz)) { // elements[0][0] is the largest diagonal term
|
|
|
|
if (xx< epsilon) {
|
|
|
|
x = 0;
|
|
|
|
y = 0.7071;
|
|
|
|
z = 0.7071;
|
|
|
|
} else {
|
|
|
|
x = Math::sqrt(xx);
|
|
|
|
y = xy/x;
|
|
|
|
z = xz/x;
|
|
|
|
}
|
|
|
|
} else if (yy > zz) { // elements[1][1] is the largest diagonal term
|
|
|
|
if (yy< epsilon) {
|
|
|
|
x = 0.7071;
|
|
|
|
y = 0;
|
|
|
|
z = 0.7071;
|
|
|
|
} else {
|
|
|
|
y = Math::sqrt(yy);
|
|
|
|
x = xy/y;
|
|
|
|
z = yz/y;
|
|
|
|
}
|
|
|
|
} else { // elements[2][2] is the largest diagonal term so base result on this
|
|
|
|
if (zz< epsilon) {
|
|
|
|
x = 0.7071;
|
|
|
|
y = 0.7071;
|
|
|
|
z = 0;
|
|
|
|
} else {
|
|
|
|
z = Math::sqrt(zz);
|
|
|
|
x = xz/z;
|
|
|
|
y = yz/z;
|
|
|
|
}
|
|
|
|
}
|
|
|
|
r_axis=Vector3(x,y,z);
|
|
|
|
r_angle=angle;
|
|
|
|
return;
|
|
|
|
}
|
|
|
|
// as we have reached here there are no singularities so we can handle normally
|
|
|
|
double s = Math::sqrt((elements[1][2] - elements[2][1])*(elements[1][2] - elements[2][1])
|
|
|
|
+(elements[2][0] - elements[0][2])*(elements[2][0] - elements[0][2])
|
2016-10-18 22:50:21 +02:00
|
|
|
+(elements[0][1] - elements[1][0])*(elements[0][1] - elements[1][0])); // s=|axis||sin(angle)|, used to normalise
|
|
|
|
|
2014-02-10 02:10:30 +01:00
|
|
|
angle = Math::acos(( elements[0][0] + elements[1][1] + elements[2][2] - 1)/2);
|
2016-10-18 22:50:21 +02:00
|
|
|
if (angle < 0) s = -s;
|
|
|
|
x = (elements[2][1] - elements[1][2])/s;
|
|
|
|
y = (elements[0][2] - elements[2][0])/s;
|
|
|
|
z = (elements[1][0] - elements[0][1])/s;
|
2014-02-10 02:10:30 +01:00
|
|
|
|
|
|
|
r_axis=Vector3(x,y,z);
|
|
|
|
r_angle=angle;
|
|
|
|
}
|
|
|
|
|
|
|
|
Matrix3::Matrix3(const Vector3& p_euler) {
|
|
|
|
|
|
|
|
set_euler( p_euler );
|
2016-03-09 00:00:52 +01:00
|
|
|
|
2014-02-10 02:10:30 +01:00
|
|
|
}
|
|
|
|
|
|
|
|
Matrix3::Matrix3(const Quat& p_quat) {
|
|
|
|
|
|
|
|
real_t d = p_quat.length_squared();
|
|
|
|
real_t s = 2.0 / d;
|
|
|
|
real_t xs = p_quat.x * s, ys = p_quat.y * s, zs = p_quat.z * s;
|
|
|
|
real_t wx = p_quat.w * xs, wy = p_quat.w * ys, wz = p_quat.w * zs;
|
|
|
|
real_t xx = p_quat.x * xs, xy = p_quat.x * ys, xz = p_quat.x * zs;
|
|
|
|
real_t yy = p_quat.y * ys, yz = p_quat.y * zs, zz = p_quat.z * zs;
|
2016-03-09 00:00:52 +01:00
|
|
|
set( 1.0 - (yy + zz), xy - wz, xz + wy,
|
|
|
|
xy + wz, 1.0 - (xx + zz), yz - wx,
|
2014-02-10 02:10:30 +01:00
|
|
|
xz - wy, yz + wx, 1.0 - (xx + yy)) ;
|
|
|
|
|
|
|
|
}
|
|
|
|
|
|
|
|
Matrix3::Matrix3(const Vector3& p_axis, real_t p_phi) {
|
2016-10-18 22:50:21 +02:00
|
|
|
// Rotation matrix from axis and angle, see https://en.wikipedia.org/wiki/Rotation_matrix#Rotation_matrix_from_axis_and_angle
|
2014-02-10 02:10:30 +01:00
|
|
|
|
|
|
|
Vector3 axis_sq(p_axis.x*p_axis.x,p_axis.y*p_axis.y,p_axis.z*p_axis.z);
|
|
|
|
|
|
|
|
real_t cosine= Math::cos(p_phi);
|
|
|
|
real_t sine= Math::sin(p_phi);
|
|
|
|
|
|
|
|
elements[0][0] = axis_sq.x + cosine * ( 1.0 - axis_sq.x );
|
2016-10-18 22:50:21 +02:00
|
|
|
elements[0][1] = p_axis.x * p_axis.y * ( 1.0 - cosine ) - p_axis.z * sine;
|
|
|
|
elements[0][2] = p_axis.z * p_axis.x * ( 1.0 - cosine ) + p_axis.y * sine;
|
2014-02-10 02:10:30 +01:00
|
|
|
|
2016-10-18 22:50:21 +02:00
|
|
|
elements[1][0] = p_axis.x * p_axis.y * ( 1.0 - cosine ) + p_axis.z * sine;
|
2014-02-10 02:10:30 +01:00
|
|
|
elements[1][1] = axis_sq.y + cosine * ( 1.0 - axis_sq.y );
|
2016-10-18 22:50:21 +02:00
|
|
|
elements[1][2] = p_axis.y * p_axis.z * ( 1.0 - cosine ) - p_axis.x * sine;
|
2014-02-10 02:10:30 +01:00
|
|
|
|
2016-10-18 22:50:21 +02:00
|
|
|
elements[2][0] = p_axis.z * p_axis.x * ( 1.0 - cosine ) - p_axis.y * sine;
|
|
|
|
elements[2][1] = p_axis.y * p_axis.z * ( 1.0 - cosine ) + p_axis.x * sine;
|
2014-02-10 02:10:30 +01:00
|
|
|
elements[2][2] = axis_sq.z + cosine * ( 1.0 - axis_sq.z );
|
|
|
|
|
|
|
|
}
|
|
|
|
|