SimpleAscentPropagator Class |
Inheritance HierarchyAGI.Foundation.InfrastructureDefinitionalObject
AGI.Foundation.PropagatorsCartesianOnePointPropagator
AGI.Foundation.PropagatorsSimpleAscentPropagator
Namespace: AGI.Foundation.Propagators
Assembly: AGI.Foundation.Models (in AGI.Foundation.Models.dll) Version: 24.2.419.0 (24.2.419.0)
SyntaxThe SimpleAscentPropagator type exposes the following members.
Constructors| Name | Description | |
|---|---|---|
 | SimpleAscentPropagator | Initializes a new instance. |
Properties| Name | Description | |
|---|---|---|
 | AscentType |
Gets or sets the interpolation type for the ascent. Use the quartic type when specifying an initial acceleration.
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| BurnoutEpoch |
Gets or sets the time of burnout, at which the launch vehicle will be at BurnoutPosition.
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| BurnoutPosition |
Gets or sets the location of burnout.
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| BurnoutVelocityAzimuth |
Gets or sets the burnout velocity's azimuth. This defaults to zero.
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| BurnoutVelocityFightPathAngle |
Gets or sets the burnout velocity's flight path angle. This defaults to zero.
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| BurnoutVelocityFrame |
Gets or sets which reference frame the burnout velocity is specified in.
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| BurnoutVelocityMagnitude |
Gets or sets the burnout velocity magnitude in the reference frame of the CentralBody as indicated by
the property BurnoutVelocityFrame. This defaults to zero m/s.
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| CentralBody |
Gets or sets the central body to be used for the launch segment.
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| InitialAcceleration |
Gets or sets the initial acceleration at launch. The AscentType type must be set to quartic to use. This defaults to zero m/s^2.
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| Interpolator |
Gets or sets the interpolator used to get values between the analytical points. This defaults to
LagrangePolynomialApproximation and order 7. It is recommended that this property be left as the default.
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| 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.) |
| LaunchEpoch |
Gets or sets the epoch at which launch occurs.
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| LaunchPosition |
Gets or sets the position on/near the CentralBody where the launch takes place.
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| NumberOfSamplePoints |
Gets or sets the number of points to be sampled on the interpolation spline.
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| Order |
Gets or sets the order of the motion produced by the propagator. This may be up to jerk (order 3).
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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.
(Overrides CartesianOnePointPropagatorGetEvaluator(EvaluatorGroup).) |
| 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.) |
 | MixedFixedPositionAndInertialVelocityToMotionFixed |
This method computes the burnout motion in the fixed frame of the CentralBody from mixed inertial velocity/fixed position input.
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| 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.) |
Events| Name | Description | |
|---|---|---|
 | WarningsHandler |
An event that can be used to check for/handle warnings produced during propagation.
If not set, the propagator will throw an InvalidOperationException if a warning is encountered.
The error text in the exception is the same as the summary documentation for each boolean property in the events arguments class.
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See Also