TwoBodyStateTransitionMatrixPropagator Class |
Inheritance HierarchyAGI.Foundation.InfrastructureDefinitionalObject
AGI.Foundation.PropagatorsTwoBodyStateTransitionMatrixPropagator
Namespace: AGI.Foundation.Propagators
Assembly: AGI.Foundation.Models (in AGI.Foundation.Models.dll) Version: 24.3.420.0 (24.3.420.0)
SyntaxThe TwoBodyStateTransitionMatrixPropagator type exposes the following members.
Constructors| Name | Description | |
|---|---|---|
 | TwoBodyStateTransitionMatrixPropagator | |
| TwoBodyStateTransitionMatrixPropagator(TwoBodyPropagator) |
Initializes a new instance.
|
| TwoBodyStateTransitionMatrixPropagator(JulianDate, MotionCartesian, Double) |
Initializes a new instance.
|
Properties| Name | Description | |
|---|---|---|
 | Epoch |
Gets or sets the Julian date at which the initial conditions are defined.
|
| GravitationalParameter |
Gets or sets the gravitational parameter for the central body around which to propagate.
|
| InitialConditions |
Gets or sets the orbital state of the spacecraft at the Epoch.
|
| IsFrozen |
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.) |
Methods| Name | Description | |
|---|---|---|
| Clone |
Clones this object using the specified context.
(Overrides DefinitionalObjectClone(CopyContext).) |
| EnumerateDependencies |
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.) |
| Equals | Determines whether the specified object is equal to the current object. (Inherited from Object.) |
| Freeze |
Freezes this object. Further attempts to modify it will result
in an ObjectFrozenException.
(Inherited from DefinitionalObject.) |
| GetDefinitionHashCode |
Gets a hash code representing the definition of this object.
(Inherited from DefinitionalObject.) |
| GetEvaluator | 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. |
| GetEvaluator(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. |
| GetHashCode | Serves as the default hash function. (Inherited from Object.) |
| GetType | Gets the Type of the current instance. (Inherited from Object.) |
| IsSameDefinition |
Determines if this object has the same definition as another object.
(Inherited from DefinitionalObject.) |
| ToString | Returns a string that represents the current object. (Inherited from Object.) |
See Also