new_thea/Embedded/libraries/Adafruit_BNO055/utility/quaternion.h

/*
    Inertial Measurement Unit Maths Library
    Copyright (C) 2013-2014  Samuel Cowen
        www.camelsoftware.com

    Bug fixes and cleanups by Gé Vissers (gvissers@gmail.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 <math.h>
#include <stdint.h>
#include <stdlib.h>
#include <string.h>

#include "matrix.h"

namespace imu {

class Quaternion {
public:
  Quaternion() : _w(1.0), _x(0.0), _y(0.0), _z(0.0) {}

  Quaternion(double w, double x, double y, double z)
      : _w(w), _x(x), _y(y), _z(z) {}

  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 {
    return sqrt(_w * _w + _x * _x + _y * _y + _z * _z);
  }

  void normalize() {
    double mag = magnitude();
    *this = this->scale(1 / mag);
  }

  Quaternion conjugate() const { return Quaternion(_w, -_x, -_y, -_z); }

  void fromAxisAngle(const 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(const Matrix<3> &m) {
    double tr = m.trace();

    double S;
    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, double &angle) const {
    double 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(double 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(const Vector<2> &v) const {
    return rotateVector(Vector<3>(v.x(), v.y()));
  }

  Vector<3> rotateVector(const Vector<3> &v) const {
    Vector<3> qv(_x, _y, _z);
    Vector<3> t = qv.cross(v) * 2.0;
    return v + t * _w + qv.cross(t);
  }

  Quaternion operator*(const Quaternion &q) const {
    return Quaternion(_w * q._w - _x * q._x - _y * q._y - _z * q._z,
                      _w * q._x + _x * q._w + _y * q._z - _z * q._y,
                      _w * q._y - _x * q._z + _y * q._w + _z * q._x,
                      _w * q._z + _x * q._y - _y * q._x + _z * q._w);
  }

  Quaternion operator+(const Quaternion &q) const {
    return Quaternion(_w + q._w, _x + q._x, _y + q._y, _z + q._z);
  }

  Quaternion operator-(const Quaternion &q) const {
    return Quaternion(_w - q._w, _x - q._x, _y - q._y, _z - q._z);
  }

  Quaternion operator/(double scalar) const {
    return Quaternion(_w / scalar, _x / scalar, _y / scalar, _z / scalar);
  }

  Quaternion operator*(double scalar) const { return scale(scalar); }

  Quaternion scale(double scalar) const {
    return Quaternion(_w * scalar, _x * scalar, _y * scalar, _z * scalar);
  }

private:
  double _w, _x, _y, _z;
};

} // namespace imu

#endif