Uses of Class
agi.foundation.Motion1

Packages that use Motion1

Package	Description
agi.foundation	Contains commonly used types.
agi.foundation.access	Contains types used in performing access calculations.
agi.foundation.aircraftpropagation	Contains types for propagating an aircraft through various maneuvers subject to flight phase performance models and wind effects.
agi.foundation.celestial	Contains types used in modeling characteristics of celestial objects and celestial phenomena.
agi.foundation.communications.antennas	Contains types for representing antennas, defining gain patterns, and processing electromagnetic signals.
agi.foundation.communications.signalprocessing	Contains types for representing communication hardware and processing electromagnetic signals.
agi.foundation.coordinates	Contains types for quantifying and converting between various coordinate representations.
agi.foundation.geometry	Contains types for expressing the motion of fundamental geometric objects such as points, axes, and reference frames; the manner in which they are related; and transformations between representations.
agi.foundation.geometry.shapes	Contains types for representing geometric shapes such as curves, surfaces, and solids.
agi.foundation.infrastructure	Contains types which support various aspects of the DME Component Libraries infrastructure.
agi.foundation.numericalmethods	Contains general numerical algorithms.
agi.foundation.numericalmethods.advanced	Contains additional advanced numerical algorithms and supporting types.
agi.foundation.propagators	Contains types used in producing the state of an object from a known element set.
agi.foundation.propagators.advanced	Contains types used to create more specialized propagation scenarios.
agi.foundation.routedesign	Contains types for creating simple routes by specifying procedures at points of interest, how to connect them, and what height and speed to use along the route.
agi.foundation.routedesign.advanced	Contains types used to define immutable geometry and configuration for routes.
agi.foundation.segmentpropagation	Contains types for modeling a trajectory in segments, where the type of propagation varies for each segment.

Uses of Motion1 in agi.foundation

Methods in agi.foundation that return Motion1

Modifier and Type	Method and Description
abstract Motion1<T>	MotionEvaluator1.evaluate(JulianDate date, int order) Evaluates the function.
abstract Motion1<TDependent>	Function2.evaluate(TIndependent x, int order) Evaluates the function.

Methods in agi.foundation that return types with arguments of type Motion1

Modifier and Type	Method and Description
List<Motion1<T>>	ImmutableDateMotionCollection1.getMotions() Gets the list of motion instances in this collection.
List<Motion1<T>>	IDateMotionCollection1.getMotions() Gets the list of motion instances in this collection.
List<Motion1<T>>	DateMotionCollection1.getMotions() Gets the list of motion instances in this collection.

Methods in agi.foundation with parameters of type Motion1

Modifier and Type	Method and Description
void	IDateMotionCollection1.add(JulianDate date, Motion1<T> motion) Adds an item to the collection.
void	DateMotionCollection1.add(JulianDate date, Motion1<T> motion) Adds an item to the collection.
static <T> boolean	Motion1.equals(Motion1<T> left, Motion1<T> right) Returns true if the two instances are exactly equal.
static <T> boolean	Motion1.equals(Motion1<T> left, Motion1<T> right) Returns true if the two instances are exactly equal.
boolean	Motion1.equalsType(Motion1<T> other) Indicates whether another instance of this type is exactly equal to this instance.
void	DateMotionCollection1.insertItem(int index, JulianDate date, Motion1<T> motion) Inserts an item at a particular index.
static <T> boolean	Motion1.notEquals(Motion1<T> left, Motion1<T> right) Returns true if the two instances are not exactly equal.
static <T> boolean	Motion1.notEquals(Motion1<T> left, Motion1<T> right) Returns true if the two instances are not exactly equal.
void	IDateMotionCollection1.setItem(int index, JulianDate date, Motion1<T> motion) Sets an item at a particular index.
void	DateMotionCollection1.setItem(int index, JulianDate date, Motion1<T> motion) Sets an item at a particular index.

Uses of Motion1 in agi.foundation.access

Methods in agi.foundation.access with parameters of type Motion1

Modifier and Type	Method and Description
static JulianDate	AccessConstraintSampling.getNextStepFromRelativeMotion(JulianDate epoch, Motion1<Cartesian> relativeMotion, double maximumAngularMotion) Computes an appropriate next sample step based on the relative motion between the two platforms involved in the Access computation and a maximum relative motion per step.

Uses of Motion1 in agi.foundation.aircraftpropagation

Methods in agi.foundation.aircraftpropagation that return Motion1

Modifier and Type	Method and Description
Motion1<Cartesian>	AircraftStateElementConverter.convertState(double[] overallState) Convert the raw state into a Cartesian and its derivatives.
Motion1<double[]>	AircraftStateElementConverter.getElementFromState(double[] overallState) Produces this state element's values and their derivatives from the overall raw state.
Motion1<Cartesian>	AircraftReferenceState.toMotionInFixedFrame(WindModel winds) Converts the reference state of the aircraft into motion with respect to the fixed frame of the HeightReferenceSurface (get / set).

Methods in agi.foundation.aircraftpropagation with parameters of type Motion1

Modifier and Type	Method and Description
boolean	AircraftStateElementConverter.adjustStateFromElement(double[] overallRawState, Motion1<double[]> stateElementValues) Adjust the subset of the overall raw state corresponding to this element to new values.
<T> boolean	AircraftStateElementConverter.adjustStateWithType(double[] overallRawState, Motion1<T> newStateElement) Adjust the subset of the raw state corresponding to this element to new values.
static void	AircraftMotionIntegrationPoint.configureIndicesOnEvaluator(EvaluatorGroup group, AircraftMotionIntegrationPoint point, Motion1<int[]> stateInputIndices) This is called by PropagationStateElement instances using PointPropagationParameter so that the element can update the indices used to identify the individual values corresponding to this point in the state during evaluation.

Constructors in agi.foundation.aircraftpropagation with parameters of type Motion1

Constructor and Description
AircraftStateElementConverter(String identification, Motion1<int[]> stateIndices, Cartesian initialPosition, Cartesian initialVelocity, Ellipsoid ellipsoid) Initializes a new instance.
AircraftStateElementConverter(String identification, Motion1<int[]> stateIndices, Cartesian initialPosition, Cartesian initialVelocity, Ellipsoid ellipsoid, Motion1<double[]> weights) Initializes a new instance.
AircraftStateElementConverter(String identification, Motion1<int[]> stateIndices, Cartesian initialPosition, Cartesian initialVelocity, Ellipsoid ellipsoid, Motion1<double[]> weights) Initializes a new instance.

Uses of Motion1 in agi.foundation.celestial

Methods in agi.foundation.celestial with parameters of type Motion1

Modifier and Type	Method and Description
static boolean	CentralBodyIntersection.doesIntersect(Motion1<Cartesian> motionOne, Motion1<Cartesian> motionTwo, int numberOfRevs, double geocentricRadiusOfIntersection, double gravitationalParameter) Determines if an orbit will intersect the planet specified by the corresponding gravitational parameter and geocentric radius of intersection.
static boolean	CentralBodyIntersection.doesIntersect(Motion1<Cartesian> motionOne, Motion1<Cartesian> motionTwo, int numberOfRevs, double geocentricRadiusOfIntersection, double gravitationalParameter) Determines if an orbit will intersect the planet specified by the corresponding gravitational parameter and geocentric radius of intersection.

Uses of Motion1 in agi.foundation.communications.antennas

Methods in agi.foundation.communications.antennas that return Motion1

Modifier and Type	Method and Description
Motion1<Double>	SphericalTabularGainData.evaluate(Cartesian direction, int order) Evaluate the gain given the cartesian direction expressed in the antennas axes.

Uses of Motion1 in agi.foundation.communications.signalprocessing

Methods in agi.foundation.communications.signalprocessing that return Motion1

Modifier and Type	Method and Description
Motion1<Double>	VariableGainAmplifierBackoffPolynomial.evaluate(Double x, int order) Evaluate the backoff polynomial given the normalized input power.

Uses of Motion1 in agi.foundation.coordinates

Methods in agi.foundation.coordinates that return Motion1

Modifier and Type	Method and Description
static Motion1<LongitudeLatitudeRadius>	LongitudeLatitudeRadius.convertMotion(Motion1<Cartesian> motion, int order) Converts the motion given in terms of a set of Cartesian coordinates to motion of the corresponding set of LongitudeLatitudeRadius coordinates.
static Motion1<AzimuthElevationRange>	AzimuthElevationRange.convertMotion(Motion1<Cartesian> topographic, int order) Construct a Motion<Cartesian> which represents the motion expressed with AzimuthElevationRange values and derivatives.
static Motion1<Cartesian>	Cartesian.convertMotion(Motion1<LongitudeLatitudeRadius> motion, int order) Converts the motion given in terms of a set of LongitudeLatitudeRadius coordinates to motion of the corresponding set of Cartesian coordinates.
static Motion1<Double>	UnitCartesian.dihedralAngle(Motion2<UnitCartesian,Cartesian> motFrom, Motion2<UnitCartesian,Cartesian> motTo, Motion2<UnitCartesian,Cartesian> motAxis, int order) Calculates the scalar dihedral angle (and derivatives) of the three given values with Cartesian derivative information.
<T> Motion1<T>	ITimeBasedState.getMotion(String elementIdentification) Returns the Motion1 of the requested elementIdentification.
<T> Motion1<T>	BasicState.getMotion(String elementIdentification) Returns the Motion1 of the requested elementIdentification.
Motion1<Cartesian>	KinematicTransformation.getTranslationalMotion() Gets the translational portion of this transformation.
Motion1<Cartesian>	ModifiedKeplerianElements.toCartesian() Returns a cartesian representation of these orbital elements.
Motion1<Cartesian>	KozaiIzsakMeanElements.toCartesian() Returns an osculating Cartesian representation of these mean orbital elements.
Motion1<Cartesian>	KeplerianElements.toCartesian() Returns a cartesian representation of these orbital elements.
Motion1<Cartesian>	EquinoctialElements.toCartesian() Converts this set of equinoctial elements to a cartesian position and velocity.
Motion1<Cartesian>	DelaunayElements.toCartesian() Converts this set of Delaunay elements to a cartesian position and velocity.
static Motion1<RotationVectorAngularVelocity>	RotationVectorAngularVelocity.toMotionRotationVectorAngularVelocity(Motion2<UnitQuaternion,Cartesian> motionUnitQuaternionCartesian, int order) Converts a Motion<UnitQuaternion, Cartesian> to a Motion<RotationVectorAngularVelocity>.
Motion1<Cartesian>	HelmertTransformation.transform(Motion1<Cartesian> motion) Transforms the motion observed in the A frame to the B frame.
Motion1<Cartesian>	KinematicTransformation.transform(Motion1<Cartesian> motion) Transforms the motion observed in the A frame to the B frame.
Motion1<Cartesian>	HelmertTransformation.transform(Motion1<Cartesian> motion, int order) Transforms the motion observed in the A frame to the B frame.
Motion1<Cartesian>	KinematicTransformation.transform(Motion1<Cartesian> motion, int order) Transforms the motion observed in the A frame to the B frame.
static Motion1<Cartesian>	RotationalTransformation.transform(Motion2<UnitQuaternion,Cartesian> rotationalTransformation, Motion1<Cartesian> motion, int order) Transforms the vector observed in the A axes to the B axes.

Methods in agi.foundation.coordinates with parameters of type Motion1

Modifier and Type	Method and Description
<T> void	IAdjustableState.addStateElementMotion(String elementIdentification, Motion1<T> motion) Adds a Motion{T} element to this state.
<T> void	BasicState.addStateElementMotion(String elementIdentification, Motion1<T> motion) Adds a Motion{T} element to this state.
static Motion2<UnitCartesian,Cartesian>	UnitCartesian.convertMotion(Motion1<Cartesian> motion, int order) Converts the motion given in terms of a set of Cartesian coordinates to motion of the corresponding set of UnitCartesian coordinates.
static Motion1<LongitudeLatitudeRadius>	LongitudeLatitudeRadius.convertMotion(Motion1<Cartesian> motion, int order) Converts the motion given in terms of a set of Cartesian coordinates to motion of the corresponding set of LongitudeLatitudeRadius coordinates.
static Motion1<AzimuthElevationRange>	AzimuthElevationRange.convertMotion(Motion1<Cartesian> topographic, int order) Construct a Motion<Cartesian> which represents the motion expressed with AzimuthElevationRange values and derivatives.
static Motion1<Cartesian>	Cartesian.convertMotion(Motion1<LongitudeLatitudeRadius> motion, int order) Converts the motion given in terms of a set of LongitudeLatitudeRadius coordinates to motion of the corresponding set of Cartesian coordinates.
static Motion2<UnitQuaternion,Cartesian>	AlignedConstrained.getMotion(Motion1<Cartesian> principal, Motion1<Cartesian> reference, int order) Given a principal and reference vector expressed in the same set of axes, computes a transformation that will take a vector expressed in that set of axes and expresses it in the aligned-constrained axes.
static Motion2<UnitQuaternion,Cartesian>	AlignedConstrained.getMotion(Motion1<Cartesian> principal, Motion1<Cartesian> reference, int order) Given a principal and reference vector expressed in the same set of axes, computes a transformation that will take a vector expressed in that set of axes and expresses it in the aligned-constrained axes.
<T> void	ITimeBasedState.modifyMotion(String elementIdentification, Motion1<T> newValue) Modifies this instance of ITimeBasedState with the Motion1 of the specified elementIdentification updated.
<T> void	BasicState.modifyMotion(String elementIdentification, Motion1<T> newValue) Modifies this instance of ITimeBasedState with the Motion1 of the specified elementIdentification updated.
static Motion2<UnitQuaternion,Cartesian>	RotationVectorAngularVelocity.toMotionUnitQuaternionCartesian(Motion1<RotationVectorAngularVelocity> motionRotationVectorAngularVelocity, int order) Converts a Motion<RotationVectorAngularVelocity> to a Motion<UnitQuaternion, Cartesian>.
Motion1<Cartesian>	HelmertTransformation.transform(Motion1<Cartesian> motion) Transforms the motion observed in the A frame to the B frame.
Motion1<Cartesian>	KinematicTransformation.transform(Motion1<Cartesian> motion) Transforms the motion observed in the A frame to the B frame.
Motion1<Cartesian>	HelmertTransformation.transform(Motion1<Cartesian> motion, int order) Transforms the motion observed in the A frame to the B frame.
Motion1<Cartesian>	KinematicTransformation.transform(Motion1<Cartesian> motion, int order) Transforms the motion observed in the A frame to the B frame.
static Motion1<Cartesian>	RotationalTransformation.transform(Motion2<UnitQuaternion,Cartesian> rotationalTransformation, Motion1<Cartesian> motion, int order) Transforms the vector observed in the A axes to the B axes.

Constructors in agi.foundation.coordinates with parameters of type Motion1

Constructor and Description
DelaunayElements(Motion1<Cartesian> motion, double gravitationalParameter) Initializes a new instance from the specified cartesian motion and gravitational constant.
DelaunayElements(Motion1<Cartesian> motion, double gravitationalParameter, double eccentricityTolerance, double inclinationTolerance) Initializes a new instance from the specified cartesian motion and gravitational constant.
EquinoctialElements(Motion1<Cartesian> motion, double gravitationalParameter) Initializes a new instance from the specified cartesian motion and gravitational constant.
KeplerianElements(Motion1<Cartesian> motion, double gravitationalParameter) Initializes a new instance from the specified Cartesian motion and gravitational parameter.
KeplerianElements(Motion1<Cartesian> motion, double gravitationalParameter, double eccentricityTolerance, double inclinationTolerance) Initializes a new instance from the specified cartesian motion and gravitational constant.
KinematicTransformation(Motion1<Cartesian> translationalMotion, Motion2<UnitQuaternion,Cartesian> rotationalMotion) Initializes a new instance from the specified translational and rotational motion.
KozaiIzsakMeanElements(Motion1<Cartesian> motion, double gravitationalParameter, double j2UnnormalizedValue, double referenceDistance) Initializes a set of Kozai-Izsak mean elements from the specified Cartesian motion.
ModifiedKeplerianElements(Motion1<Cartesian> motion, double gravitationalParameter) Initializes a new instance from the specified Cartesian motion and gravitational constant.
ModifiedKeplerianElements(Motion1<Cartesian> motion, double gravitationalParameter, double eccentricityTolerance, double inclinationTolerance) Initializes a new instance from the specified Cartesian motion and gravitational parameter.

Uses of Motion1 in agi.foundation.geometry

Methods in agi.foundation.geometry that return Motion1

Modifier and Type	Method and Description
Motion1<Cartesian>	InternationalTerrestrialReferenceFrameTransformer.getRotation() Gets the off-diagonal components of the skew-symmetric rotation matrix that is used to transform between the ITRFs, and the rate at which it changes after the Epoch (get / set).
Motion1<Double>	InternationalTerrestrialReferenceFrameTransformer.getScaling() Gets a small number that is added to one to form the diagonal components of the skew-symmetric rotation matrix that is used to transform between the ITRFs, and the rate at which it changes after the Epoch (get / set).
Motion1<Cartesian>	InternationalTerrestrialReferenceFrameTransformer.getTranslation() Gets the constant position offset between the two ITRFs, and the rate at which it changes after the Epoch (get / set).

Methods in agi.foundation.geometry with parameters of type Motion1

Modifier and Type	Method and Description
static Motion2<UnitQuaternion,Cartesian>	AxesEastNorthUp.computeFixedToEastNorthUpRotation(Ellipsoid shape, Motion1<Cartesian> fixedReferencePoint, int order) Computes the rotation from the central body's fixed axes to a set of east-north-up axes based on a specified reference point.
static Motion2<UnitQuaternion,Cartesian>	AxesNorthEastDown.computeFixedToNorthEastDownRotation(Ellipsoid shape, Motion1<Cartesian> fixedReferencePoint, int order) Computes the rotation from the central body's fixed axes to a set of north-east-down axes based on a specified reference point.
static Motion2<UnitQuaternion,Cartesian>	AxesAlignedConstrained.computeTransformation(Motion1<Cartesian> principal, AxisIndicator principalAxis, Motion1<Cartesian> reference, AxisIndicator referenceAxis, int order) Given a principal and reference vector expressed in the same set of axes, computes a transformation that will take a vector expressed in that set of axes and expresses it in the aligned-constrained axes.
static Motion2<UnitQuaternion,Cartesian>	AxesAlignedConstrained.computeTransformation(Motion1<Cartesian> principal, AxisIndicator principalAxis, Motion1<Cartesian> reference, AxisIndicator referenceAxis, int order) Given a principal and reference vector expressed in the same set of axes, computes a transformation that will take a vector expressed in that set of axes and expresses it in the aligned-constrained axes.
static Motion2<UnitQuaternion,Cartesian>	AxesAlignedConstrained.computeTransformation(Motion1<Cartesian> principal, Motion1<Cartesian> reference, int order) Given a principal and reference vector expressed in the same set of axes, computes a transformation that will take a vector expressed in that set of axes and expresses it in the aligned-constrained axes.
static Motion2<UnitQuaternion,Cartesian>	AxesAlignedConstrained.computeTransformation(Motion1<Cartesian> principal, Motion1<Cartesian> reference, int order) Given a principal and reference vector expressed in the same set of axes, computes a transformation that will take a vector expressed in that set of axes and expresses it in the aligned-constrained axes.
static void	AxesPropagationParameter.configureIndicesOnEvaluator(EvaluatorGroup group, AxesPropagationParameter axes, Motion1<int[]> stateInputIndices) This is called by PropagationStateElement instances using AxesPropagationParameter so that the element can update the indices used to identify the individual values corresponding to this axes in the state during evaluation.
static void	DynamicMatrixPropagationParameter.configureIndicesOnEvaluator(EvaluatorGroup group, DynamicMatrixPropagationParameter matrix, Motion1<int[]> stateInputIndices) This is called by PropagationStateElement instances using DynamicMatrixPropagationParameter so that the element can update the indices used to identify the individual values corresponding to this scalar in the state during evaluation.
static void	PointPropagationParameter.configureIndicesOnEvaluator(EvaluatorGroup group, PointPropagationParameter point, Motion1<int[]> stateInputIndices) This is called by PropagationStateElement instances using PointPropagationParameter so that the element can update the indices used to identify the individual values corresponding to this point in the state during evaluation.
static void	VectorPropagationParameter.configureIndicesOnEvaluator(EvaluatorGroup group, VectorPropagationParameter vector, Motion1<int[]> stateInputIndices) This is called by PropagationStateElement instances using VectorPropagationParameter so that the element can update the indices used to identify the individual values corresponding to this vector in the state during evaluation.
void	InternationalTerrestrialReferenceFrameTransformer.setRotation(Motion1<Cartesian> value) Sets the off-diagonal components of the skew-symmetric rotation matrix that is used to transform between the ITRFs, and the rate at which it changes after the Epoch (get / set).
void	InternationalTerrestrialReferenceFrameTransformer.setScaling(Motion1<Double> value) Sets a small number that is added to one to form the diagonal components of the skew-symmetric rotation matrix that is used to transform between the ITRFs, and the rate at which it changes after the Epoch (get / set).
void	InternationalTerrestrialReferenceFrameTransformer.setTranslation(Motion1<Cartesian> value) Sets the constant position offset between the two ITRFs, and the rate at which it changes after the Epoch (get / set).

Constructors in agi.foundation.geometry with parameters of type Motion1

Constructor and Description
InternationalTerrestrialReferenceFrameTransformer(String from, String to, JulianDate epoch, Motion1<Cartesian> translation, Motion1<Double> scaling, Motion1<Cartesian> rotation) Initializes a new instance.
InternationalTerrestrialReferenceFrameTransformer(String from, String to, JulianDate epoch, Motion1<Cartesian> translation, Motion1<Double> scaling, Motion1<Cartesian> rotation) Initializes a new instance.
InternationalTerrestrialReferenceFrameTransformer(String from, String to, JulianDate epoch, Motion1<Cartesian> translation, Motion1<Double> scaling, Motion1<Cartesian> rotation) Initializes a new instance.

Uses of Motion1 in agi.foundation.geometry.shapes

Methods in agi.foundation.geometry.shapes that return Motion1

Modifier and Type	Method and Description
Motion1<Cartographic>	Ellipsoid.cartesianToCartographic(Motion1<Cartesian> cartesianMotion, int order) Converts the motion given in terms of cartesian coordinates to motion in cartographic coordinates.
Motion1<Cartesian>	Ellipsoid.cartographicToCartesian(Motion1<Cartographic> cartographicMotion, int order) Converts the motion given in terms of planetodetic cartographic coordinates to motion in cartesian coordinates.
Motion1<Double>	EllipsoidGeodesic.headingMotion(Cartographic location, double groundSpeed) Provides the heading and rate of change of heading at a location on the geodesic.
Motion1<Cartesian>	EllipsoidRhumbLine.surfaceMotion(double distance, double groundSpeed, double groundAcceleration) Converts the motion given in terms of motion on the rhumb line curve to motion of the surface point.
Motion1<Cartesian>	EllipsoidGeodesic.surfaceMotion(double distance, double groundSpeed, double groundAcceleration) Converts the motion given in terms of motion on the geodesic curve to motion of the surface point.
Motion1<Cartesian>	Ellipsoid.surfaceProjection(Motion1<Cartesian> motion, int order) Computes the projection of the cartesian motion onto the ellipsoid surface.
Motion1<Cartesian>	Ellipsoid.surfaceProjectionCartographic(Motion1<Cartographic> cartographicMotion, int order) Computes the projection of the cartographic motion onto the ellipsoid surface.

Methods in agi.foundation.geometry.shapes with parameters of type Motion1

Modifier and Type	Method and Description
Motion1<Cartographic>	Ellipsoid.cartesianToCartographic(Motion1<Cartesian> cartesianMotion, int order) Converts the motion given in terms of cartesian coordinates to motion in cartographic coordinates.
Motion1<Cartesian>	Ellipsoid.cartographicToCartesian(Motion1<Cartographic> cartographicMotion, int order) Converts the motion given in terms of planetodetic cartographic coordinates to motion in cartesian coordinates.
Motion2<UnitCartesian,Cartesian>	Ellipsoid.surfaceNormalMotion(Motion1<Cartesian> surfaceMotion, int order) Converts the motion given in terms of a surface point to motion of the surface normal vector.
Motion1<Cartesian>	Ellipsoid.surfaceProjection(Motion1<Cartesian> motion, int order) Computes the projection of the cartesian motion onto the ellipsoid surface.
Motion1<Cartesian>	Ellipsoid.surfaceProjectionCartographic(Motion1<Cartographic> cartographicMotion, int order) Computes the projection of the cartographic motion onto the ellipsoid surface.

Uses of Motion1 in agi.foundation.infrastructure

Methods in agi.foundation.infrastructure that return Motion1

Modifier and Type	Method and Description
Motion1<TResult>	ParameterizedMotionEvaluator.evaluate(JulianDate date, int order) Evaluates this parameterized evaluator.
Motion1<T>	CachingMotionEvaluator1.evaluate(JulianDate date, int order) Evaluates the function, first checking for a cached result corresponding to date and order.
Motion1<TResult>	ParameterizedMotionEvaluator1.evaluate(JulianDate date, int order, TParameter1 parameter1) Evaluates this parameterized evaluator.
Motion1<TResult>	ParameterizedMotionEvaluator2.evaluate(JulianDate date, int order, TParameter1 parameter1, TParameter2 parameter2) Evaluates this parameterized evaluator.
Motion1<TResult>	ParameterizedMotionEvaluator3.evaluate(JulianDate date, int order, TParameter1 parameter1, TParameter2 parameter2, TParameter3 parameter3) Evaluates this parameterized evaluator.
Motion1<TResult>	ParameterizedMotionEvaluator4.evaluate(JulianDate date, int order, TParameter1 parameter1, TParameter2 parameter2, TParameter3 parameter3, TParameter4 parameter4) Evaluates this parameterized evaluator.
Motion1<TResult>	ParameterizedMotionEvaluator5.evaluate(JulianDate date, int order, TParameter1 parameter1, TParameter2 parameter2, TParameter3 parameter3, TParameter4 parameter4, TParameter5 parameter5) Evaluates this parameterized evaluator.
Motion1<TResult>	ParameterizedMotionEvaluator6.evaluate(JulianDate date, int order, TParameter1 parameter1, TParameter2 parameter2, TParameter3 parameter3, TParameter4 parameter4, TParameter5 parameter5, TParameter6 parameter6) Evaluates this parameterized evaluator.
Motion1<TResult>	ParameterizedMotionEvaluator7.evaluate(JulianDate date, int order, TParameter1 parameter1, TParameter2 parameter2, TParameter3 parameter3, TParameter4 parameter4, TParameter5 parameter5, TParameter6 parameter6, TParameter7 parameter7) Evaluates this parameterized evaluator.

Uses of Motion1 in agi.foundation.numericalmethods

Methods in agi.foundation.numericalmethods that return Motion1

Modifier and Type	Method and Description
Motion1<Double>	RealValuedScalarFunctionAdapter.evaluate(T x, int order) Evaluates the function.

Uses of Motion1 in agi.foundation.numericalmethods.advanced

Methods in agi.foundation.numericalmethods.advanced that return Motion1

Modifier and Type	Method and Description
Motion1<Matrix>	PartialDerivativesEvaluator.evaluate(JulianDate date, int order) PartialDerivativeEvaluators only calculate zeroth order values, this method returns a Motion1 of order zero regardless of the requested order.

Uses of Motion1 in agi.foundation.propagators

Methods in agi.foundation.propagators that return Motion1

Modifier and Type	Method and Description
<T> Motion1<T>	PropagationStateConverter.convertState(String elementID, double[] state) Convert a given state and auxiliary values to useful data based on the given element.
Motion1<double[]>	PropagationVector.getAdaptiveWeights() Gets the weights to be applied to the scalar values when computing the error which determines how to adapt the step size during integration.
Motion1<Double>	PropagationScalar.getAdaptiveWeights() Gets the weights to be applied to the scalar values when computing the error which determines how to adapt the step size during integration.
Motion1<double[]>	PropagationStateConverter.getElementFromState(String elementID, double[] overallState) Produces this state element's values and their derivatives from the overall raw state.
Motion1<Cartesian>	BallisticTrajectoryInformation.getFinalConditionsFixed() Gets the position and velocity at the FinalTime (get), in the CentralBody (get) fixed frame.
Motion1<Cartesian>	BallisticTrajectoryInformation.getFinalConditionsInertial() Gets the position and velocity at the FinalTime (get), in the CentralBody (get) inertial frame.
Motion1<Cartesian>	LambertResult.getFinalPositionMotion() Gets the final motion as computed by the LambertOrbitSolver.
Motion1<Cartesian>	TwoBodyStateTransitionMatrixPropagator.getInitialConditions() Gets the orbital state of the spacecraft at the Epoch (get / set).
Motion1<Cartesian>	TwoBodyPropagator.getInitialConditions() Gets the orbital elements from which to propagate.
Motion1<Cartesian>	BallisticTrajectoryInformation.getInitialConditionsFixed() Gets the position and velocity at the InitialTime (get), in the CentralBody (get) fixed frame.
Motion1<Cartesian>	BallisticTrajectoryInformation.getInitialConditionsInertial() Gets the position and velocity at the InitialTime (get), in the CentralBody (get) inertial frame.
Motion1<Cartesian>	SinglePointStoppablePropagatorDefinition.getInitialMotion() Gets the optional initial position and velocity for this propagator.
Motion1<Cartesian>	LambertResult.getInitialPositionMotion() Gets the initial motion as computed by the LambertOrbitSolver.
Motion1<Cartesian>	PropagationVector.getInitialState() Gets the initial vector and its derivatives up to the order of the VectorDerivative (get / set).
Motion1<Double>	PropagationScalar.getInitialState() Gets the initial value and its derivatives up to the order of the ScalarDerivative (get / set).
<T> Motion1<T>	NumericalPropagatorState.getMotion(String elementIdentification) Gets the Motion1 stored in this state specified by the elementIdentification.
Motion1<double[]>	NumericalPropagatorState.getMotionOfDoubleArray(String elementIdentification) Gets the motion of the specified elementIdentification as an array of doubles.
Motion1<Cartesian>	InitialOrbitSolverResults.getPosition1Motion() Gets the motion for the first position in the orbit.
Motion1<Cartesian>	InitialOrbitSolverResults.getPosition2Motion() Gets the motion for the second position in the orbit.
Motion1<Cartesian>	InitialOrbitSolverResults.getPosition3Motion() Gets the motion for the third position in the orbit.
static Motion1<Cartesian>	SimpleAscentPropagator.mixedFixedPositionAndInertialVelocityToMotionFixed(boolean isAtPole, KinematicTransformation inertialToFixed, Cartesian position, double inertialSpeed, double inertialFlightPathAngle, double inertialAzimuth) This method computes the burnout motion in the fixed frame of the CentralBody (get / set) from mixed inertial velocity/fixed position input.
Motion1<Cartesian>	InitialOrbitSolver.solve(Cartesian position1, Cartesian position2, Cartesian position3) Solves the initial orbit determination problem using the Gibbs method.
Motion1<Cartesian>	InitialOrbitSolver.solve(Cartesian position1, Cartesian position2, Cartesian position3, JulianDate time1, JulianDate time2, JulianDate time3) Solves the initial orbit determination problem using the Herrick-Gibbs method for closely spaced positions.

Methods in agi.foundation.propagators with parameters of type Motion1

Modifier and Type	Method and Description
<T> boolean	PropagationStateConverter.adjustState(String elementID, double[] stateToAdjust, Motion1<T> newStateValues) Adjust a subset of the overall state to new values based on the requested element.
boolean	PropagationStateConverter.adjustStateFromElement(String elementID, double[] overallRawState, Motion1<double[]> stateElementValues) Adjust the subset of the overall raw state corresponding to this element to new values.
PropagationStateElementConverter	PropagationNewtonianPoint.getConverter(EvaluatorGroup group, Motion1<int[]> stateInputIndices) Gets an instance of an output type which can convert the output of propagation back into the native type of this state element.
PropagationStateElementConverter	PropagationEulerianAxes.getConverter(EvaluatorGroup group, Motion1<int[]> stateInputIndices) Gets an instance of an output type which can convert the output of propagation back into the native type of this state element.
PropagationStateElementConverter	StateTransitionMatrix.getConverter(EvaluatorGroup group, Motion1<int[]> stateInputIndices) Gets an instance of an output type which can convert the output of propagation back into the native type of this state element.
PropagationStateElementConverter	PropagationVector.getConverter(EvaluatorGroup group, Motion1<int[]> stateInputIndices) Gets an instance of an output type which can convert the output of propagation back into the native type of this state element.
PropagationStateElementConverter	PropagationScalar.getConverter(EvaluatorGroup group, Motion1<int[]> stateInputIndices) Gets an instance of an output type which can convert the output of propagation back into the native type of this state element.
protected abstract PointEvaluator	SinglePointStoppablePropagator.initializePropagationPoint(JulianDate date, Motion1<Cartesian> motion) Creates the PointEvaluator that will be sampled for propagation.
<T> void	NumericalPropagatorState.modifyMotion(String elementIdentification, Motion1<T> newValue) Modifies this instance of ITimeBasedState with the Motion1 of the specified elementIdentification updated.
SinglePointStoppablePropagatorResults	SinglePointStoppablePropagator.propagateUntilStop(JulianDate initialDate, Motion1<Cartesian> initialState, IntegrationSense direction, ITrackCalculationProgress progressTracker) Propagates a Point forward in time from the initial conditions.
SinglePointStoppablePropagatorResults	SinglePointStoppablePropagator.propagateUntilStop(JulianDate initialDate, Motion1<Cartesian> initialState, Iterable<? extends StoppingConditionEvaluator> conditions, IntegrationSense direction, int outputSparsity, ITrackCalculationProgress progressTracker) Propagates a Point forward in time from the initial conditions.
void	PropagationVector.setAdaptiveWeights(Motion1<double[]> value) Sets the weights to be applied to the scalar values when computing the error which determines how to adapt the step size during integration.
void	PropagationScalar.setAdaptiveWeights(Motion1<Double> value) Sets the weights to be applied to the scalar values when computing the error which determines how to adapt the step size during integration.
void	LambertResult.setFinalPositionMotion(Motion1<Cartesian> value) Sets the final motion as computed by the LambertOrbitSolver.
void	TwoBodyStateTransitionMatrixPropagator.setInitialConditions(Motion1<Cartesian> value) Sets the orbital state of the spacecraft at the Epoch (get / set).
void	TwoBodyPropagator.setInitialConditions(Motion1<Cartesian> value) Sets the orbital elements from which to propagate.
void	SinglePointStoppablePropagatorDefinition.setInitialMotion(Motion1<Cartesian> value) Sets the optional initial position and velocity for this propagator.
void	LambertResult.setInitialPositionMotion(Motion1<Cartesian> value) Sets the initial motion as computed by the LambertOrbitSolver.
void	PropagationVector.setInitialState(Motion1<Cartesian> value) Sets the initial vector and its derivatives up to the order of the VectorDerivative (get / set).
void	PropagationScalar.setInitialState(Motion1<Double> value) Sets the initial value and its derivatives up to the order of the ScalarDerivative (get / set).

Constructors in agi.foundation.propagators with parameters of type Motion1

Constructor and Description
InitialOrbitSolverResults(Motion1<Cartesian> position1Motion, Motion1<Cartesian> position2Motion, Motion1<Cartesian> position3Motion) Initializes the results data container.
InitialOrbitSolverResults(Motion1<Cartesian> position1Motion, Motion1<Cartesian> position2Motion, Motion1<Cartesian> position3Motion) Initializes the results data container.
InitialOrbitSolverResults(Motion1<Cartesian> position1Motion, Motion1<Cartesian> position2Motion, Motion1<Cartesian> position3Motion) Initializes the results data container.
J2Propagator(JulianDate orbitEpoch, ReferenceFrame referenceFrame, Motion1<Cartesian> initialConditions, double gravitationalParameter, double j2UnnormalizedValue, double referenceDistance) Initializes a new instance.
J4Propagator(JulianDate orbitEpoch, ReferenceFrame referenceFrame, Motion1<Cartesian> initialConditions, double gravitationalParameter, double j2UnnormalizedValue, double j4UnnormalizedValue, double referenceDistance) Initializes a new instance.
TwoBodyPropagator(JulianDate orbitEpoch, ReferenceFrame referenceFrame, Motion1<Cartesian> initialConditions, double gravitationalParameter) Initializes a new instance.
TwoBodyStateTransitionMatrixPropagator(JulianDate epoch, Motion1<Cartesian> initialConditions, double gravitationalParameter) Initializes a new instance.

Uses of Motion1 in agi.foundation.propagators.advanced

Methods in agi.foundation.propagators.advanced that return Motion1

Modifier and Type	Method and Description
Motion1<RotationVectorAngularVelocity>	RotationVectorAngularVelocityStateElementConverter.convertState(double[] overallState) Convert the raw state into a RotationVectorAngularVelocity and its derivatives.
Motion1<Matrix>	MatrixStateElementConverter.convertState(double[] overallState) Convert the raw state into a Matrix and its derivatives.
Motion1<Cartesian>	CartesianStateElementConverter.convertState(double[] overallState) Convert the raw state into a Cartesian and its derivatives.
abstract <T> Motion1<T>	PropagationStateElementConverter.convertState(double[] overallState) Convert the raw state into this instance's TypeOfOutput (get) and its derivatives.
abstract <T> Motion1<T>	AuxiliaryStateElementConverter.convertState(double[] auxiliaryState) Convert the raw auxiliary state into this instance's TypeOfOutput (get) and its derivatives.
Motion1<double[]>	PropagationStateElementConverter.getAdaptiveWeights() Gets the weights to be applied to the state elements when computing the error which determines how to adapt the step size during integration.
Motion1<double[]>	RotationVectorAngularVelocityStateElementConverter.getElementFromState(double[] overallState) Produces this state element's values and their derivatives from the overall raw state.
abstract Motion1<double[]>	PropagationStateElementConverter.getElementFromState(double[] overallState) Produces this state element's values and their derivatives from the overall raw state.
Motion1<double[]>	MatrixStateElementConverter.getElementFromState(double[] overallState) Produces this state element's values and their derivatives from the overall raw state.
Motion1<double[]>	CartesianStateElementConverter.getElementFromState(double[] overallState) Produces this state element's values and their derivatives from the overall raw state.
Motion1<double[]>	PropagationStateElementConverter.getInitialState() Gets the initial values of this element of the state and their derivatives.
Motion1<int[]>	PropagationStateElementConverter.getStateIndices() Gets the indices locating each variable of this element within the overall state.

Methods in agi.foundation.propagators.advanced with parameters of type Motion1

Modifier and Type	Method and Description
boolean	RotationVectorAngularVelocityStateElementConverter.adjustStateFromElement(double[] overallRawState, Motion1<double[]> stateElementValues) Adjust the subset of the overall raw state corresponding to this element to new values.
abstract boolean	PropagationStateElementConverter.adjustStateFromElement(double[] overallRawState, Motion1<double[]> stateElementValues) Adjust the subset of the overall raw state corresponding to this element to new values.
boolean	MatrixStateElementConverter.adjustStateFromElement(double[] overallRawState, Motion1<double[]> stateElementValues) Adjust the subset of the overall raw state corresponding to this element to new values.
boolean	CartesianStateElementConverter.adjustStateFromElement(double[] overallRawState, Motion1<double[]> stateElementValues) Adjust the subset of the overall raw state corresponding to this element to new values.
<T> boolean	RotationVectorAngularVelocityStateElementConverter.adjustStateWithType(double[] overallRawState, Motion1<T> newStateElement) Adjust the subset of the raw state corresponding to this element to new values.
abstract <T> boolean	PropagationStateElementConverter.adjustStateWithType(double[] overallRawState, Motion1<T> newStateElement) Adjust the subset of the raw state corresponding to this element to new values.
<T> boolean	MatrixStateElementConverter.adjustStateWithType(double[] overallRawState, Motion1<T> newStateElement) Adjust the subset of the raw state corresponding to this element to new values.
<T> boolean	CartesianStateElementConverter.adjustStateWithType(double[] overallRawState, Motion1<T> newStateElement) Adjust the subset of the raw state corresponding to this element to new values.
abstract PropagationStateElementConverter	PropagationStateElement.getConverter(EvaluatorGroup group, Motion1<int[]> stateInputIndices) Gets an instance of an output type which can convert the output of propagation back into the native type of this state element.
protected void	PropagationStateElementConverter.setAdaptiveWeights(Motion1<double[]> value) Sets the weights to be applied to the state elements when computing the error which determines how to adapt the step size during integration.

Constructors in agi.foundation.propagators.advanced with parameters of type Motion1

Constructor and Description
CartesianStateElementConverter(String identification, Motion1<int[]> stateIndices, Motion1<Cartesian> initialState) Initializes a new instance.
CartesianStateElementConverter(String identification, Motion1<int[]> stateIndices, Motion1<Cartesian> initialState) Initializes a new instance.
CartesianStateElementConverter(String identification, Motion1<int[]> stateIndices, Motion1<Cartesian> initialState, Motion1<double[]> weights) Initializes a new instance.
CartesianStateElementConverter(String identification, Motion1<int[]> stateIndices, Motion1<Cartesian> initialState, Motion1<double[]> weights) Initializes a new instance.
CartesianStateElementConverter(String identification, Motion1<int[]> stateIndices, Motion1<Cartesian> initialState, Motion1<double[]> weights) Initializes a new instance.
MatrixStateElementConverter(String identification, Motion1<int[]> stateIndices, Motion1<Matrix> initialState) Initializes a new instance.
MatrixStateElementConverter(String identification, Motion1<int[]> stateIndices, Motion1<Matrix> initialState) Initializes a new instance.
MatrixStateElementConverter(String identification, Motion1<int[]> stateIndices, Motion1<Matrix> initialState, Motion1<Matrix> weights) Initializes a new instance.
MatrixStateElementConverter(String identification, Motion1<int[]> stateIndices, Motion1<Matrix> initialState, Motion1<Matrix> weights) Initializes a new instance.
MatrixStateElementConverter(String identification, Motion1<int[]> stateIndices, Motion1<Matrix> initialState, Motion1<Matrix> weights) Initializes a new instance.
PropagationStateElementConverter(String identification, Motion1<int[]> stateIndices, Motion1<double[]> initialState) Initializes a new instance.
PropagationStateElementConverter(String identification, Motion1<int[]> stateIndices, Motion1<double[]> initialState) Initializes a new instance.
PropagationStateElementConverter(String identification, Motion1<int[]> stateIndices, Motion1<double[]> initialState, Motion1<double[]> weights) Initializes a new instance.
PropagationStateElementConverter(String identification, Motion1<int[]> stateIndices, Motion1<double[]> initialState, Motion1<double[]> weights) Initializes a new instance.
PropagationStateElementConverter(String identification, Motion1<int[]> stateIndices, Motion1<double[]> initialState, Motion1<double[]> weights) Initializes a new instance.
RotationVectorAngularVelocityStateElementConverter(String identification, Motion1<int[]> stateIndices, Motion1<RotationVectorAngularVelocity> initialState) Initializes a new instance.
RotationVectorAngularVelocityStateElementConverter(String identification, Motion1<int[]> stateIndices, Motion1<RotationVectorAngularVelocity> initialState) Initializes a new instance.
RotationVectorAngularVelocityStateElementConverter(String identification, Motion1<int[]> stateIndices, Motion1<RotationVectorAngularVelocity> initialState, Motion1<double[]> weights) Initializes a new instance.
RotationVectorAngularVelocityStateElementConverter(String identification, Motion1<int[]> stateIndices, Motion1<RotationVectorAngularVelocity> initialState, Motion1<double[]> weights) Initializes a new instance.
RotationVectorAngularVelocityStateElementConverter(String identification, Motion1<int[]> stateIndices, Motion1<RotationVectorAngularVelocity> initialState, Motion1<double[]> weights) Initializes a new instance.

Uses of Motion1 in agi.foundation.routedesign

Methods in agi.foundation.routedesign with parameters of type Motion1

Modifier and Type	Method and Description
static HeadingAtWaypointProcedure	HeadingAtWaypointProcedure.getFinalFromNextState(CentralBody centralBody, Motion1<Cartesian> stateInFixedFrame, ProfileDynamics dynamics, double turningRadius) Creates an instance of the procedure to represent a final state for a route based on a given state (position and velocity) in the FixedFrame (get / set) of the CentralBody.
static HeadingAtWaypointProcedure	HeadingAtWaypointProcedure.getInitialFromPreviousState(CentralBody centralBody, Motion1<Cartesian> stateInFixedFrame, ProfileDynamics dynamics, double turningRadius) Creates an instance of the procedure to represent an initial state for a route based on a given state (position and velocity) in the FixedFrame (get / set) of the CentralBody.

Uses of Motion1 in agi.foundation.routedesign.advanced

Methods in agi.foundation.routedesign.advanced that return Motion1

Modifier and Type	Method and Description
Motion1<Double>	ParametricRouteSegment.getHeading(Duration time, int order) Get the heading and rates at a given time since the start of the segment.
abstract Motion1<Double>	SurfaceSegment.getHeading(Motion1<Double> distanceAlongPath, int order) Get the heading and its derivatives, in radians and radians/meter.
Motion1<Double>	SurfaceCurveSegment.getHeading(Motion1<Double> distanceAlongPath, int order) Get the heading and its derivatives, in radians and radians/meter.
Motion1<Double>	PartialSurfaceSegment.getHeading(Motion1<Double> distanceAlongPath, int order) Get the heading and its derivatives, in radians and radians/meter.
Motion1<Double>	DegenerateSurfaceSegment.getHeading(Motion1<Double> distanceAlongPath, int order) Get the heading and its derivatives, in radians and radians/meter.
Motion1<Double>	CompositeSurfaceSegment.getHeading(Motion1<Double> distanceAlongPath, int order) Get the heading and its derivatives, in radians and radians/meter.
Motion1<Double>	StandardTransitionProfileSegment.getHeight(Duration time, int order) Get the value for the height above the TerrainProvider height reference specified by the StandardTransitionProfileSegment.getHeightReference(agi.foundation.time.Duration) method at the given time.
abstract Motion1<Double>	ProfileSegment.getHeight(Duration time, int order) Get the value for the height above the TerrainProvider height reference specified by the ProfileSegment.getHeightReference(agi.foundation.time.Duration) method at the given time.
Motion1<Double>	ConstantHeightSegment.getHeight(Duration time, int order) Get the value for the height above the TerrainProvider height reference specified by the ConstantHeightSegment.getHeightReference(agi.foundation.time.Duration) method at the given time.
Motion1<Double>	CompositeProfileSegment.getHeight(Duration time, int order) Get the value for the height above the TerrainProvider height reference specified by the CompositeProfileSegment.getHeightReference(agi.foundation.time.Duration) method at the given time.
Motion1<Double>	ParametricRouteSegment.getHeight(Duration time, int order, TerrainProvider heightReference) Get the height and rates at a given time since the start of the segment.
Motion1<Double>	StandardTransitionProfileSegment.getSurfaceMotion(Duration time, int order) Get the value for the arc length and its derivatives along the surface path, in meters and seconds.
abstract Motion1<Double>	ProfileSegment.getSurfaceMotion(Duration time, int order) Get the value for the arc length and its derivatives along the surface path, in meters and seconds.
Motion1<Double>	ConstantHeightSegment.getSurfaceMotion(Duration time, int order) Get the value for the arc length and its derivatives along the surface path, in meters and seconds.
Motion1<Double>	CompositeProfileSegment.getSurfaceMotion(Duration time, int order) Get the value for the arc length and its derivatives along the surface path, in meters and seconds.
Motion1<Cartesian>	ParametricRouteSegment.traverseFixed(Duration time, int order) Produces the position along the route in the fixed frame of the SurfaceShape (get) as a function of time from the start of this segment of the route.

Methods in agi.foundation.routedesign.advanced with parameters of type Motion1

Modifier and Type	Method and Description
abstract Motion1<Double>	SurfaceSegment.getHeading(Motion1<Double> distanceAlongPath, int order) Get the heading and its derivatives, in radians and radians/meter.
Motion1<Double>	SurfaceCurveSegment.getHeading(Motion1<Double> distanceAlongPath, int order) Get the heading and its derivatives, in radians and radians/meter.
Motion1<Double>	PartialSurfaceSegment.getHeading(Motion1<Double> distanceAlongPath, int order) Get the heading and its derivatives, in radians and radians/meter.
Motion1<Double>	DegenerateSurfaceSegment.getHeading(Motion1<Double> distanceAlongPath, int order) Get the heading and its derivatives, in radians and radians/meter.
Motion1<Double>	CompositeSurfaceSegment.getHeading(Motion1<Double> distanceAlongPath, int order) Get the heading and its derivatives, in radians and radians/meter.

Uses of Motion1 in agi.foundation.segmentpropagation

Methods in agi.foundation.segmentpropagation that return types with arguments of type Motion1

Modifier and Type	Method and Description
<T> ArrayList<Motion1<T>>	SegmentResults.getMotionCollection(String element) Returns a collection of Motion1 of the element from the EphemerisForOverallTrajectory (get).
static <T> ArrayList<Motion1<T>>	SegmentResults.getMotionCollection(String element, List<ITimeBasedState> states) Gets a List of the element.