Uses of Interface
org.orekit.propagation.numerical.TimeDerivativesEquations
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Packages that use TimeDerivativesEquations Package Description org.orekit.forces This package provides the interface for force models that will be used by theNumericalPropagator
, 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. -
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Uses of TimeDerivativesEquations in org.orekit.forces
Methods in org.orekit.forces with parameters of type TimeDerivativesEquations Modifier and Type Method Description default void
ForceModel. addContribution(SpacecraftState s, TimeDerivativesEquations adder)
Compute the contribution of the force model to the perturbing acceleration. -
Uses of TimeDerivativesEquations in org.orekit.forces.gravity
Methods in org.orekit.forces.gravity with parameters of type TimeDerivativesEquations Modifier and Type Method Description void
NewtonianAttraction. addContribution(SpacecraftState s, TimeDerivativesEquations adder)
Compute the contribution of the force model to the perturbing acceleration. -
Uses of TimeDerivativesEquations in org.orekit.forces.maneuvers
Methods in org.orekit.forces.maneuvers with parameters of type TimeDerivativesEquations Modifier and Type Method Description void
Maneuver. addContribution(SpacecraftState s, TimeDerivativesEquations adder)
Compute the contribution of the force model to the perturbing acceleration.
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