Class NumericalOrbitDynamics

• Defined in File dynamics.h

Inheritance Relationships

Base Type

• public lupnt::IOrbitDynamics (Class IOrbitDynamics)

Derived Types

• public lupnt::CartesianTwoBodyDynamics (Class CartesianTwoBodyDynamics)

• public lupnt::J2CartTwoBodyDynamics (Class J2CartTwoBodyDynamics)

• public lupnt::J2KeplerianDynamics (Class J2KeplerianDynamics)

• public lupnt::MoonMeanDynamics (Class MoonMeanDynamics)

• public lupnt::NBodyDynamics< T > (Template Class NBodyDynamics)

Class Documentation

class NumericalOrbitDynamics : public lupnt::IOrbitDynamics

Subclassed by lupnt::CartesianTwoBodyDynamics, lupnt::J2CartTwoBodyDynamics, lupnt::J2KeplerianDynamics, lupnt::MoonMeanDynamics, lupnt::NBodyDynamics< T >

Public Functions

NumericalOrbitDynamics(ODE odefunc = nullptr, IntegratorType integ = default_integrator)

void SetTimeStep(Real dt)

Real GetTimeStep() const

void SetODEFunction(ODE odefunc)

inline void SetIntegratorParams(IntegratorParams params)

virtual Vec6 Propagate(const Vec6 &x0, Real t0, Real tf, Mat6d *stm = nullptr) override

virtual MatX6 Propagate(const Vec6 &x0, Real t0, const VecX &tf, bool progress = false) override

virtual Vec6 ComputeRates(Real t, const Vec6 &x) const = 0

virtual OrbitState PropagateState(const OrbitState &state, Real t0, Real tf, Mat6d *stm = nullptr) override = 0

VecX Propagate(const VecX &x0, Real t0, Real tf, MatXd *stm = nullptr) override

Vec6 Propagate(const Vec6 &x0, Real t0, Real tf, Mat6d *stm = nullptr) = 0

MatX6 Propagate(const Vec6 &x0, Real t0, const VecX &tf, bool progress = false) = 0

MatX6 Propagate(const MatX6 &x0, Real t0, Real tf)