px4_autopilot/matrix/Euler.hpp

/**
 * @file Euler.hpp
 *
 * All rotations and axis systems follow the right-hand rule
 *
 * An instance of this class defines a rotation from coordinate frame 1 to coordinate frame 2.
 * It follows the convention of a 3-2-1 intrinsic Tait-Bryan rotation sequence.
 * In order to go from frame 1 to frame 2 we apply the following rotations consecutively.
 * 1) We rotate about our initial Z axis by an angle of _psi.
 * 2) We rotate about the newly created Y' axis by an angle of _theta.
 * 3) We rotate about the newly created X'' axis by an angle of _phi.
 *
 * @author James Goppert <james.goppert@gmail.com>
 */

#pragma once

#include "math.hpp"

namespace matrix
{

template <typename Type>
class Dcm;

template <typename Type>
class Quaternion;

/**
 * Euler angles class
 *
 * This class describes the rotation from frame 1
 * to frame 2 via 3-2-1 intrinsic Tait-Bryan rotation sequence.
 */
template<typename Type>
class Euler : public Vector<Type, 3>
{
public:
    /**
     * Standard constructor
     */
    Euler() = default;

    /**
     * Copy constructor
     *
     * @param other vector to copy
     */
    Euler(const Vector<Type, 3> &other) :
        Vector<Type, 3>(other)
    {
    }

    /**
     * Constructor from Matrix31
     *
     * @param other Matrix31 to copy
     */
    Euler(const Matrix<Type, 3, 1> &other) :
        Vector<Type, 3>(other)
    {
    }

    /**
     * Constructor from euler angles
     *
     * Instance is initialized from an 3-2-1 intrinsic Tait-Bryan
     * rotation sequence representing transformation from frame 1
     * to frame 2.
     *
     * @param phi_ rotation angle about X axis
     * @param theta_ rotation angle about Y axis
     * @param psi_ rotation angle about Z axis
     */
    Euler(Type phi_, Type theta_, Type psi_) : Vector<Type, 3>()
    {
        phi() = phi_;
        theta() = theta_;
        psi() = psi_;
    }

    /**
     * Constructor from DCM matrix
     *
     * Instance is set from Dcm representing transformation from
     * frame 2 to frame 1.
     * This instance will hold the angles defining the 3-2-1 intrinsic
     * Tait-Bryan rotation sequence from frame 1 to frame 2.
     *
     * @param dcm Direction cosine matrix
    */
    Euler(const Dcm<Type> &dcm)
    {
        theta() = asin(-dcm(2, 0));

        if ((fabs(theta() - Type(M_PI / 2))) < Type(1.0e-3)) {
            phi() = 0;
            psi() = atan2(dcm(1, 2), dcm(0, 2));

        } else if ((fabs(theta() + Type(M_PI / 2))) < Type(1.0e-3)) {
            phi() = 0;
            psi() = atan2(-dcm(1, 2), -dcm(0, 2));

        } else {
            phi() = atan2(dcm(2, 1), dcm(2, 2));
            psi() = atan2(dcm(1, 0), dcm(0, 0));
        }
    }

    /**
     * Constructor from quaternion instance.
     *
     * Instance is set from a quaternion representing transformation
     * from frame 2 to frame 1.
     * This instance will hold the angles defining the 3-2-1 intrinsic
     * Tait-Bryan rotation sequence from frame 1 to frame 2.
     *
     * @param q quaternion
    */
    Euler(const Quaternion<Type> &q) : Vector<Type, 3>(Euler(Dcm<Type>(q)))
    {
    }

    inline Type phi() const
    {
        return (*this)(0);
    }
    inline Type theta() const
    {
        return (*this)(1);
    }
    inline Type psi() const
    {
        return (*this)(2);
    }

    inline Type &phi()
    {
        return (*this)(0);
    }
    inline Type &theta()
    {
        return (*this)(1);
    }
    inline Type &psi()
    {
        return (*this)(2);
    }

};

using Eulerf = Euler<float>;
using Eulerd = Euler<double>;

} // namespace matrix

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