TwoBodyPropagator Class |
Inheritance HierarchyAGI.Foundation.InfrastructureDefinitionalObject
AGI.Foundation.PropagatorsCartesianOnePointPropagator
AGI.Foundation.PropagatorsTwoBodyPropagator
Namespace: AGI.Foundation.Propagators
Assembly: AGI.Foundation.Models (in AGI.Foundation.Models.dll) Version: 24.2.419.0 (24.2.419.0)
SyntaxThe TwoBodyPropagator type exposes the following members.
Constructors| Name | Description | |
|---|---|---|
 | TwoBodyPropagator(JulianDate, ReferenceFrame, DelaunayElements) |
Initializes a new instance.
|
| TwoBodyPropagator(JulianDate, ReferenceFrame, EquinoctialElements) |
Initializes a new instance.
|
| TwoBodyPropagator(JulianDate, ReferenceFrame, KeplerianElements) |
Initializes a new instance.
|
| TwoBodyPropagator(JulianDate, ReferenceFrame, ModifiedKeplerianElements) |
Initializes a new instance.
|
| TwoBodyPropagator(JulianDate, ReferenceFrame, MotionCartesian, Double) |
Initializes a new instance.
|
Properties| Name | Description | |
|---|---|---|
 | GravitationalParameter |
Gets the gravitational parameter for the central body around which to propagate.
|
| InitialConditions |
Gets or sets the orbital elements from which to propagate.
|
| 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.) |
| OrbitEpoch |
Gets or sets the Julian date at which the InitialConditions of
the orbit are defined.
|
| ReferenceFrame |
Gets or sets the reference frame in which the ephemeris is produced.
|
Methods| Name | Description | |
|---|---|---|
| Clone |
Clones this object using the specified context.
(Overrides DefinitionalObjectClone(CopyContext).) |
| CreatePoint |
Creates a Point that represents the motion produced by this propagator.
(Inherited from CartesianOnePointPropagator.) |
| 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.
(Overrides DefinitionalObjectEnumerateDependencies(DependencyEnumerator).) |
| 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 at individual dates. This evaluator propagates the orbit state. The result of evaluating will be a MotionT corresponding to the orbital state at the given JulianDate expressed in the propagator's ReferenceFrame. 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 at individual dates. This evaluator propagates the orbit state from InitialConditions at OrbitEpoch based on the GravitationalParameter. The result of evaluating will be a Motion<Cartesian> corresponding to the orbital position and velocity at the given JulianDate expressed in the propagator's ReferenceFrame. |
| 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.) |
| Propagate(JulianDate, JulianDate, Duration, Int32, ReferenceFrame) | Calculates position (and zero or more derivatives) for regular time steps over an interval. Note: when propagating, 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. |
| Propagate(JulianDate, JulianDate, Duration, Int32, ReferenceFrame, ITrackCalculationProgress) | Calculates position (and zero or more derivatives) for regular time steps over an interval. 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. |
| ToString | Returns a string that represents the current object. (Inherited from Object.) |
See Also