physics::orbit::trajectory< T > Struct Template Reference

Describes the trajectory of an orbit with Chebyshev polynomials. More...

#include <trajectory.hpp>

Public Member Functions
math::vec3< T >	position (T t) const
	Calculates the Cartesian position of a trajectory at a given time. More...

Public Attributes
T	t0
	Start time of the trajectory. More...
T	t1
	End time of the trajectory. More...
T	dt
	Time step duration. More...
std::size_t	n
	Chebyshev polynomial degree. More...
std::vector< T >	a
	Chebyshev polynomial coefficients. More...

Detailed Description

template<class T>
struct physics::orbit::trajectory< T >

Describes the trajectory of an orbit with Chebyshev polynomials.

Template Parameters

t	Real type.

Definition at line 36 of file trajectory.hpp.

Member Function Documentation

position()

template<class T >

math::vec3< T > physics::orbit::trajectory< T >::position

(

T

t

)

const

Calculates the Cartesian position of a trajectory at a given time.

Parameters

t	Time, on [t0, t1).

Returns

Trajectory position at time t.

Definition at line 63 of file trajectory.hpp.

Member Data Documentation

a

template<class T >

std::vector<T> physics::orbit::trajectory< T >::a

Chebyshev polynomial coefficients.

Definition at line 51 of file trajectory.hpp.

dt

template<class T >

T physics::orbit::trajectory< T >::dt

Time step duration.

Definition at line 45 of file trajectory.hpp.

n

template<class T >

std::size_t physics::orbit::trajectory< T >::n

Chebyshev polynomial degree.

Definition at line 48 of file trajectory.hpp.

t0

template<class T >

T physics::orbit::trajectory< T >::t0

Start time of the trajectory.

Definition at line 39 of file trajectory.hpp.

t1

template<class T >

T physics::orbit::trajectory< T >::t1

End time of the trajectory.

Definition at line 42 of file trajectory.hpp.

---

The documentation for this struct was generated from the following file:

• trajectory.hpp