BRIX5

/*

    Inertial Measurement Unit Maths Library

    Copyright (C) 2013-2014  Samuel Cowen

        www.camelsoftware.com

    This program is free software: you can redistribute it and/or modify

    it under the terms of the GNU General Public License as published by

    the Free Software Foundation, either version 3 of the License, or

    (at your option) any later version.

    This program is distributed in the hope that it will be useful,

    but WITHOUT ANY WARRANTY; without even the implied warranty of

    MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE.  See the

    GNU General Public License for more details.

    You should have received a copy of the GNU General Public License

    along with this program.  If not, see <http://www.gnu.org/licenses/>.

*/

#ifndef IMUMATH_QUATERNION_HPP

#define IMUMATH_QUATERNION_HPP

#include <stdlib.h>

#include <string.h>

#include <stdint.h>

#include <math.h>

#include "vector.h"

namespace imu

{

class Quaternion

{

public:

    Quaternion()

    {

        _w = 1.0;

        _x = _y = _z = 0.0;

    }

    Quaternion(double iw, double ix, double iy, double iz)

    {

        _w = iw;

        _x = ix;

        _y = iy;

        _z = iz;

    }

    Quaternion(double w, Vector<3> vec)

    {

        _w = w;

        _x = vec.x();

        _y = vec.y();

        _z = vec.z();

    }

    double& w()

    {

        return _w;

    }

    double& x()

    {

        return _x;

    }

    double& y()

    {

        return _y;

    }

    double& z()

    {

        return _z;

    }

    double w() const

    {

        return _w;

    }

    double x() const

    {

        return _x;

    }

    double y() const

    {

        return _y;

    }

    double z() const

    {

        return _z;

    }

    double magnitude() const

    {

        double res = (_w*_w) + (_x*_x) + (_y*_y) + (_z*_z);

        return sqrt(res);

    }

    void normalize()

    {

        double mag = magnitude();

        *this = this->scale(1/mag);

    }

    Quaternion conjugate() const

    {

        Quaternion q;

        q.w() = _w;

        q.x() = -_x;

        q.y() = -_y;

        q.z() = -_z;

        return q;

    }

    void fromAxisAngle(Vector<3> axis, double theta)

    {

        _w = cos(theta/2);

        //only need to calculate sine of half theta once

        double sht = sin(theta/2);

        _x = axis.x() * sht;

        _y = axis.y() * sht;

        _z = axis.z() * sht;

    }

    void fromMatrix(Matrix<3> m)

    {

        float tr = m(0, 0) + m(1, 1) + m(2, 2);

        float S = 0.0;

        if (tr > 0)

        {

            S = sqrt(tr+1.0) * 2;

            _w = 0.25 * S;

            _x = (m(2, 1) - m(1, 2)) / S;

            _y = (m(0, 2) - m(2, 0)) / S;

            _z = (m(1, 0) - m(0, 1)) / S;

        }

        else if ((m(0, 0) < m(1, 1))&(m(0, 0) < m(2, 2)))

        {

            S = sqrt(1.0 + m(0, 0) - m(1, 1) - m(2, 2)) * 2;

            _w = (m(2, 1) - m(1, 2)) / S;

            _x = 0.25 * S;

            _y = (m(0, 1) + m(1, 0)) / S;

            _z = (m(0, 2) + m(2, 0)) / S;

        }

        else if (m(1, 1) < m(2, 2))

        {

            S = sqrt(1.0 + m(1, 1) - m(0, 0) - m(2, 2)) * 2;

            _w = (m(0, 2) - m(2, 0)) / S;

            _x = (m(0, 1) + m(1, 0)) / S;

            _y = 0.25 * S;

            _z = (m(1, 2) + m(2, 1)) / S;

        }

        else

        {

            S = sqrt(1.0 + m(2, 2) - m(0, 0) - m(1, 1)) * 2;

            _w = (m(1, 0) - m(0, 1)) / S;

            _x = (m(0, 2) + m(2, 0)) / S;

            _y = (m(1, 2) + m(2, 1)) / S;

            _z = 0.25 * S;

        }

    }

    void toAxisAngle(Vector<3>& axis, float& angle) const

    {

        float sqw = sqrt(1-_w*_w);

        if(sqw == 0) //it's a singularity and divide by zero, avoid

            return;

        angle = 2 * acos(_w);

        axis.x() = _x / sqw;

        axis.y() = _y / sqw;

        axis.z() = _z / sqw;

    }

    Matrix<3> toMatrix() const

    {

        Matrix<3> ret;

        ret.cell(0, 0) = 1-(2*(_y*_y))-(2*(_z*_z));

        ret.cell(0, 1) = (2*_x*_y)-(2*_w*_z);

        ret.cell(0, 2) = (2*_x*_z)+(2*_w*_y);

        ret.cell(1, 0) = (2*_x*_y)+(2*_w*_z);

        ret.cell(1, 1) = 1-(2*(_x*_x))-(2*(_z*_z));

        ret.cell(1, 2) = (2*(_y*_z))-(2*(_w*_x));

        ret.cell(2, 0) = (2*(_x*_z))-(2*_w*_y);

        ret.cell(2, 1) = (2*_y*_z)+(2*_w*_x);

        ret.cell(2, 2) = 1-(2*(_x*_x))-(2*(_y*_y));

        return ret;

    }

    // Returns euler angles that represent the quaternion.  Angles are

    // returned in rotation order and right-handed about the specified

    // axes:

    //

    //   v[0] is applied 1st about z (ie, roll)

    //   v[1] is applied 2nd about y (ie, pitch)

    //   v[2] is applied 3rd about x (ie, yaw)

    //

    // Note that this means result.x() is not a rotation about x;

    // similarly for result.z().

    //

    Vector<3> toEuler() const

    {

        Vector<3> ret;

        double sqw = _w*_w;

        double sqx = _x*_x;

        double sqy = _y*_y;

        double sqz = _z*_z;

        ret.x() = atan2(2.0*(_x*_y+_z*_w),(sqx-sqy-sqz+sqw));

        ret.y() = asin(-2.0*(_x*_z-_y*_w)/(sqx+sqy+sqz+sqw));

        ret.z() = atan2(2.0*(_y*_z+_x*_w),(-sqx-sqy+sqz+sqw));

        return ret;

    }

    Vector<3> toAngularVelocity(float dt) const

    {

        Vector<3> ret;

        Quaternion one(1.0, 0.0, 0.0, 0.0);

        Quaternion delta = one - *this;

        Quaternion r = (delta/dt);

        r = r * 2;

        r = r * one;

        ret.x() = r.x();

        ret.y() = r.y();

        ret.z() = r.z();

        return ret;

    }

    Vector<3> rotateVector(Vector<2> v) const

    {

        Vector<3> ret(v.x(), v.y(), 0.0);

        return rotateVector(ret);

    }

    Vector<3> rotateVector(Vector<3> v) const

    {

        Vector<3> qv(this->x(), this->y(), this->z());

        Vector<3> t;

        t = qv.cross(v) * 2.0;

        return v + (t * _w) + qv.cross(t);

    }

    Quaternion operator * (Quaternion q) const

    {

        Quaternion ret;

        ret._w = ((_w*q._w) - (_x*q._x) - (_y*q._y) - (_z*q._z));

        ret._x = ((_w*q._x) + (_x*q._w) + (_y*q._z) - (_z*q._y));

        ret._y = ((_w*q._y) - (_x*q._z) + (_y*q._w) + (_z*q._x));

        ret._z = ((_w*q._z) + (_x*q._y) - (_y*q._x) + (_z*q._w));

        return ret;

    }

    Quaternion operator + (Quaternion q) const

    {

        Quaternion ret;

        ret._w = _w + q._w;

        ret._x = _x + q._x;

        ret._y = _y + q._y;

        ret._z = _z + q._z;

        return ret;

    }

    Quaternion operator - (Quaternion q) const

    {

        Quaternion ret;

        ret._w = _w - q._w;

        ret._x = _x - q._x;

        ret._y = _y - q._y;

        ret._z = _z - q._z;

        return ret;

    }

    Quaternion operator / (float scalar) const

    {

        Quaternion ret;

        ret._w = this->_w/scalar;

        ret._x = this->_x/scalar;

        ret._y = this->_y/scalar;

        ret._z = this->_z/scalar;

        return ret;

    }

    Quaternion operator * (float scalar) const

    {

        Quaternion ret;

        ret._w = this->_w*scalar;

        ret._x = this->_x*scalar;

        ret._y = this->_y*scalar;

        ret._z = this->_z*scalar;

        return ret;

    }

    Quaternion scale(double scalar) const

    {

        Quaternion ret;

        ret._w = this->_w*scalar;

        ret._x = this->_x*scalar;

        ret._y = this->_y*scalar;

        ret._z = this->_z*scalar;

        return ret;

    }

private:

    double _w, _x, _y, _z;

};

};

#endif