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TwoBodyStateTransitionMatrixPropagator Class

Propagates the state transition matrix of an object using a simple two-body model.
Inheritance Hierarchy
SystemObject
  AGI.Foundation.InfrastructureDefinitionalObject
    AGI.Foundation.PropagatorsTwoBodyStateTransitionMatrixPropagator

Namespace:  AGI.Foundation.Propagators
Assembly:  AGI.Foundation.Models (in AGI.Foundation.Models.dll) Version: 24.2.419.0 (24.2.419.0)
Syntax
public sealed class TwoBodyStateTransitionMatrixPropagator : DefinitionalObject

The TwoBodyStateTransitionMatrixPropagator type exposes the following members.

Constructors
Properties
  NameDescription
Public propertyEpoch
Gets or sets the Julian date at which the initial conditions are defined.
Public propertyGravitationalParameter
Gets or sets the gravitational parameter for the central body around which to propagate.
Public propertyInitialConditions
Gets or sets the orbital state of the spacecraft at the Epoch.
Public propertyIsFrozen
Gets a value indicating whether this object is frozen. A frozen object cannot be modified and an ObjectFrozenException will be thrown if an attempt is made to do so.
(Inherited from DefinitionalObject.)
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Methods
  NameDescription
Public methodClone
Clones this object using the specified context.
(Overrides DefinitionalObjectClone(CopyContext).)
Public methodEnumerateDependencies
Enumerates the dependencies of this object by calling EnumerateT(T) for each object that this object directly depends upon. Derived classes which contain additional dependencies MUST override this method, call the base implementation, and enumerate dependencies introduced by the derived class.
(Inherited from DefinitionalObject.)
Public methodEquals
Determines whether the specified object is equal to the current object.
(Inherited from Object.)
Public methodFreeze
Freezes this object. Further attempts to modify it will result in an ObjectFrozenException.
(Inherited from DefinitionalObject.)
Public methodGetDefinitionHashCode
Gets a hash code representing the definition of this object.
(Inherited from DefinitionalObject.)
Public methodGetEvaluator

Gets an evaluator that can propagate the state transition matrix to individual dates.

This evaluator propagates the orbit state transition matrix. The result of evaluating will be a Motion<Matrix> corresponding to the orbital state transition matrix at the given JulianDate.

Note: when evaluating with this evaluator, it may be more efficient to specify times using an arithmetically safe TimeStandard to avoid the need to convert in order to perform the propagation. The length of a time step may be different in different TimeStandards. So be careful when specifying times.

Public methodGetEvaluator(EvaluatorGroup)

Gets an evaluator that can propagate the state transition matrix to individual dates.

This evaluator propagates the orbit state transition matrix. The result of evaluating will be a Motion<Matrix> corresponding to the orbital state transition matrix at the given JulianDate.

Note: when evaluating with this evaluator, it may be more efficient to specify times using an arithmetically safe TimeStandard to avoid the need to convert in order to perform the propagation. The length of a time step may be different in different TimeStandards. So be careful when specifying times.

Public methodGetHashCode
Serves as the default hash function.
(Inherited from Object.)
Public methodGetType
Gets the Type of the current instance.
(Inherited from Object.)
Public methodIsSameDefinition
Determines if this object has the same definition as another object.
(Inherited from DefinitionalObject.)
Public methodToString
Returns a string that represents the current object.
(Inherited from Object.)
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See Also