AircraftStateElementConverter Class

Represents output associated with a PropagationStateElement corresponding to a set of Cartesian values. This represents the indexed state, and a means of converting the raw output information back into a Motion<Cartesian>.

Inheritance Hierarchy

SystemObject
AGI.Foundation.Propagators.AdvancedPropagationStateElementConverter
AGI.Foundation.AircraftPropagationAircraftStateElementConverter

Namespace: AGI.Foundation.AircraftPropagation
Assembly: AGI.Foundation.AircraftPropagation (in AGI.Foundation.AircraftPropagation.dll) Version: 24.2.419.0 (24.2.419.0)

Syntax

C++

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public class AircraftStateElementConverter : PropagationStateElementConverter

Public Class AircraftStateElementConverter
	Inherits PropagationStateElementConverter

public ref class AircraftStateElementConverter : public PropagationStateElementConverter

type AircraftStateElementConverter =  
    class
        inherit PropagationStateElementConverter
    end

The AircraftStateElementConverter type exposes the following members.

Constructors

	Name	Description
	AircraftStateElementConverter(AircraftStateElementConverter, CopyContext)	Initializes a new instance as a copy of an existing instance.
	AircraftStateElementConverter(String, MotionInt32, Cartesian, Cartesian, Ellipsoid)	Initializes a new instance.
	AircraftStateElementConverter(String, MotionInt32, Cartesian, Cartesian, Ellipsoid, MotionDouble)	Initializes a new instance.

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Properties

	Name	Description
	AdaptiveWeights	Gets or sets the weights to be applied to the state elements when computing the error which determines how to adapt the step size during integration. This is in addition to any weights used in the integration algorithm itself. The weights are initialized to default values of one based on the Order and Dimension of the state element. The order of the motion is one less than the Order and each array is of length Dimension. (Inherited from PropagationStateElementConverter.)
	Dimension	Gets the number of parameters (per Order) within this element. (Overrides PropagationStateElementConverterDimension.)
	Ellipsoid	Gets the ellipsoidal shape to be used in converting the propagation state elements.
	Identification	Gets the string identifying this instance in the overall output. (Inherited from PropagationStateElementConverter.)
	InitialState	Gets the initial values of this element of the state and their derivatives. The size of the initial state is its Dimension and the order of the motion is one less than the Order of the differential equation defining the derivative of this element. (Inherited from PropagationStateElementConverter.)
	IsThreadSafe	Gets a value indicating whether the methods on this instance are safe to call from multiple threads simultaneously. (Inherited from PropagationStateElementConverter.)
	Order	Gets the order of the differential equation corresponding to this element. This corresponds to one greater than the Order of the InitialState. (Inherited from PropagationStateElementConverter.)
	StateIndices	Gets the indices locating each variable of this element within the overall state. The motion represents the value of this state element and its derivatives up to but not including the Order of the differential equation defining the state's derivative. The indices will be set by the NumericalPropagatorDefinition when this element is added. (Inherited from PropagationStateElementConverter.)
	TypeOfOutput	Gets the type associated with the output of this instance. (Overrides PropagationStateElementConverterTypeOfOutput.)

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Methods

	Name	Description
	AdjustStateFromElement	Adjust the subset of the overall raw state corresponding to this element to new values. (Overrides PropagationStateElementConverterAdjustStateFromElement(Double, MotionDouble).)
	AdjustStateWithTypeT(Double, MotionT)	Adjust the subset of the raw state corresponding to this element to new values. (Overrides PropagationStateElementConverterAdjustStateWithTypeT(Double, MotionT).)
	AdjustStateWithTypeT(Double, MotionT)	Adjust the subset of the raw state corresponding to this element to new values. (Inherited from PropagationStateElementConverter.)
	Clone	Clones this object using the specified context. (Overrides PropagationStateElementConverterClone(CopyContext).)
	ConvertState(Double)	Convert the raw state into a Cartesian and its derivatives.
	ConvertStateT(Double)	Convert the raw state into this instance's Type and its derivatives. (Overrides PropagationStateElementConverterConvertStateT(Double).)
	Equals	Determines whether the specified object is equal to the current object. (Inherited from Object.)
	Finalize	Allows an object to try to free resources and perform other cleanup operations before it is reclaimed by garbage collection. (Inherited from Object.)
	GetElementFromState	Produces this state element's values and their derivatives from the overall raw state. (Overrides PropagationStateElementConverterGetElementFromState(Double).)
	GetHashCode	Serves as the default hash function. (Inherited from Object.)
	GetType	Gets the Type of the current instance. (Inherited from Object.)
	MemberwiseClone	Creates a shallow copy of the current Object. (Inherited from Object.)
	ToString	Returns a string that represents the current object. (Inherited from Object.)

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Reference

AGI.Foundation.AircraftPropagation Namespace