Uses of Package
org.orekit.propagation.numerical

Packages that use org.orekit.propagation.numerical

Package	Description
org.orekit.estimation.leastsquares	The leastsquares package provides an implementation of a batch least squares estimator engine to perform an orbit determination.
org.orekit.forces	This package provides the interface for force models that will be used by the NumericalPropagator, as well as some classical spacecraft models for surface forces (spherical, box and solar array ...).
org.orekit.forces.gravity	This package provides all gravity-related forces.
org.orekit.forces.maneuvers	This package provides models of simple maneuvers.
org.orekit.propagation.conversion	This package provides tools to convert a given propagator or a set of SpacecraftState into another propagator.
org.orekit.propagation.numerical	Top level package for numerical propagators.
org.orekit.propagation.numerical.cr3bp	Top level package for CR3BP Models used with a numerical propagator.
org.orekit.utils	This package provides useful objects.

Classes in org.orekit.propagation.numerical used by org.orekit.estimation.leastsquares

Class and Description
JacobiansMapper Mapper between two-dimensional Jacobian matrices and one-dimensional additional state arrays.

Classes in org.orekit.propagation.numerical used by org.orekit.forces

Class and Description
FieldTimeDerivativesEquations Interface summing up the contribution of several forces into orbit and mass derivatives.
TimeDerivativesEquations Interface summing up the contribution of several forces into orbit and mass derivatives.

Classes in org.orekit.propagation.numerical used by org.orekit.forces.gravity

Class and Description
FieldTimeDerivativesEquations Interface summing up the contribution of several forces into orbit and mass derivatives.
TimeDerivativesEquations Interface summing up the contribution of several forces into orbit and mass derivatives.

Classes in org.orekit.propagation.numerical used by org.orekit.forces.maneuvers

Class and Description
FieldTimeDerivativesEquations Interface summing up the contribution of several forces into orbit and mass derivatives.
TimeDerivativesEquations Interface summing up the contribution of several forces into orbit and mass derivatives.

Classes in org.orekit.propagation.numerical used by org.orekit.propagation.conversion

Class and Description
NumericalPropagator This class propagates orbits using numerical integration.

Classes in org.orekit.propagation.numerical used by org.orekit.propagation.numerical

Class and Description
AbsoluteJacobiansMapper Mapper between two-dimensional Jacobian matrices and one-dimensional additional state arrays.
GLONASSNumericalPropagator This class propagates GLONASS orbits using numerical integration.
GLONASSNumericalPropagatorBuilder This nested class aims at building a GLONASSNumericalPropagator.
JacobiansMapper Mapper between two-dimensional Jacobian matrices and one-dimensional additional state arrays.
NumericalPropagator This class propagates orbits using numerical integration.
PartialDerivativesEquations Deprecated. as of 11.1, replaced by Propagator.setupMatricesComputation(String, org.hipparchus.linear.RealMatrix, org.orekit.utils.DoubleArrayDictionary)

Classes in org.orekit.propagation.numerical used by org.orekit.propagation.numerical.cr3bp

Class and Description
NumericalPropagator This class propagates orbits using numerical integration.

Classes in org.orekit.propagation.numerical used by org.orekit.utils

Class and Description
EpochDerivativesEquations This class is a copy of AbsolutePartialDerivativesEquations The computation of the derivatives of the acceleration due to a ThirdBodyAttraction has been added.
NumericalPropagator This class propagates orbits using numerical integration.