mirror of
https://gitee.com/mirrors_PX4/PX4-Autopilot.git
synced 2026-05-02 05:04:08 +08:00
101 lines
1.9 KiB
C++
101 lines
1.9 KiB
C++
/**
|
|
* @file Euler.hpp
|
|
*
|
|
* Euler angle tait-bryan body 3-2-1
|
|
*
|
|
* @author James Goppert <james.goppert@gmail.com>
|
|
*/
|
|
|
|
#pragma once
|
|
#include <Vector.hpp>
|
|
#include <Dcm.hpp>
|
|
#include <Quaternion.hpp>
|
|
|
|
namespace matrix
|
|
{
|
|
|
|
template <typename Type>
|
|
class Dcm;
|
|
|
|
template <typename Type>
|
|
class Quaternion;
|
|
|
|
template<typename Type>
|
|
class Euler : public Vector<Type, 3>
|
|
{
|
|
public:
|
|
virtual ~Euler() {};
|
|
|
|
Euler() : Vector<Type, 3>()
|
|
{
|
|
}
|
|
|
|
Euler(const Vector<Type, 3> & other) :
|
|
Vector<Type, 3>(other)
|
|
{
|
|
}
|
|
|
|
Euler(const Matrix<Type, 3, 1> & other) :
|
|
Vector<Type, 3>(other)
|
|
{
|
|
}
|
|
|
|
Euler(Type phi_, Type theta_, Type psi_) : Vector<Type, 3>()
|
|
{
|
|
phi() = phi_;
|
|
theta() = theta_;
|
|
psi() = psi_;
|
|
}
|
|
|
|
Euler(const Dcm<Type> & dcm) : Vector<Type, 3>()
|
|
{
|
|
theta() = Type(asin(-dcm(2, 0)));
|
|
|
|
if (fabs(theta() - M_PI_2) < 1.0e-3) {
|
|
psi() = Type(atan2(dcm(1, 2) - dcm(0, 1),
|
|
dcm(0, 2) + dcm(1, 1)));
|
|
|
|
} else if (fabs(theta() + M_PI_2) < 1.0e-3) {
|
|
psi() = Type(atan2(dcm(1, 2) - dcm(0, 1),
|
|
dcm(0, 2) + dcm(1, 1)));
|
|
|
|
} else {
|
|
phi() = Type(atan2f(dcm(2, 1), dcm(2, 2)));
|
|
psi() = Type(atan2f(dcm(1, 0), dcm(0, 0)));
|
|
}
|
|
}
|
|
|
|
Euler(const Quaternion<Type> & q) :
|
|
Vector<Type, 3>()
|
|
{
|
|
*this = 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);
|
|
}
|
|
|
|
};
|
|
|
|
typedef Euler<float> Eulerf;
|
|
|
|
}; // namespace matrix
|
|
|
|
/* vim: set et fenc=utf-8 ff=unix sts=0 sw=4 ts=4 : */
|