Uses of Package
org.orekit.propagation.numerical

Packages that use org.orekit.propagation.numerical

fr.cnes.sirius.patrius.assembly.models
fr.cnes.sirius.patrius.assembly.properties
fr.cnes.sirius.patrius.forces
fr.cnes.sirius.patrius.forces.maneuvers
fr.cnes.sirius.patrius.forces.radiation
fr.cnes.sirius.patrius.propagation.numerical.multi
fr.cnes.sirius.patrius.stela.forces.drag
fr.cnes.sirius.patrius.stela.propagation
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.drag
org.orekit.forces.gravity
org.orekit.forces.gravity.tides
org.orekit.forces.gravity.variations
org.orekit.forces.maneuvers	This package provides models of simple maneuvers.
org.orekit.forces.radiation
org.orekit.forces.relativistic
org.orekit.propagation	This package provides tools to propagate orbital states with different methods.
org.orekit.propagation.events	This package provides interfaces and classes dealing with events occurring during propagation.
org.orekit.propagation.numerical
org.orekit.propagation.precomputed
org.orekit.propagation.sampling	This package provides interfaces and classes dealing with step handling during propagation.

Classes in org.orekit.propagation.numerical used by fr.cnes.sirius.patrius.assembly.models

AdditionalEquations
This interface allows users to add their own differential equations to a numerical propagator.

JacobianParametersProvider
Interface for classes that can provide parameters for computing jacobians.

Classes in org.orekit.propagation.numerical used by fr.cnes.sirius.patrius.assembly.properties

AdditionalEquations
This interface allows users to add their own differential equations to a numerical propagator.

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

Classes in org.orekit.propagation.numerical used by fr.cnes.sirius.patrius.forces

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

Classes in org.orekit.propagation.numerical used by fr.cnes.sirius.patrius.forces.maneuvers

NumericalPropagator
This class propagates SpacecraftState using numerical integration.

Classes in org.orekit.propagation.numerical used by fr.cnes.sirius.patrius.forces.radiation

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

Classes in org.orekit.propagation.numerical used by fr.cnes.sirius.patrius.propagation.numerical.multi

AdditionalEquations
This interface allows users to add their own differential equations to a numerical propagator.

AdditionalStateInfo
Utility class that describes in a minimal fashion the structure of an additional state.

AttitudeEquation
This interface allows users to add their own attitude differential equations to a numerical propagator.

Classes in org.orekit.propagation.numerical used by fr.cnes.sirius.patrius.stela.forces.drag

JacobianParametersProvider
Interface for classes that can provide parameters for computing jacobians.

Classes in org.orekit.propagation.numerical used by fr.cnes.sirius.patrius.stela.propagation

AttitudeEquation.AttitudeType

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

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.drag

JacobianParametersProvider
Interface for classes that can provide parameters for computing jacobians.

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

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.tides

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.variations

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

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.radiation

JacobianParametersProvider
Interface for classes that can provide parameters for computing jacobians.

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.relativistic

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

AdditionalEquations
This interface allows users to add their own differential equations to a numerical propagator.

AdditionalStateInfo
Utility class that describes in a minimal fashion the structure of an additional state.

AttitudeEquation.AttitudeType

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

AdditionalStateInfo
Utility class that describes in a minimal fashion the structure of an additional state.

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

AdditionalEquations
This interface allows users to add their own differential equations to a numerical propagator.

AdditionalStateInfo
Utility class that describes in a minimal fashion the structure of an additional state.

AttitudeEquation
This interface allows users to add their own attitude differential equations to a numerical propagator.

AttitudeEquation.AttitudeType

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

NumericalPropagator
This class propagates SpacecraftState using numerical integration.

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.precomputed

AdditionalStateInfo
Utility class that describes in a minimal fashion the structure of an additional state.

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

AdditionalStateInfo
Utility class that describes in a minimal fashion the structure of an additional state.

ModeHandler
Common interface for all propagator mode handlers initialization.