Uses of Class
com.irurueta.navigation.frames.ECEFPosition

Packages that use ECEFPosition

Package	Description
com.irurueta.navigation.frames	Contains frames to represent position, velocity and attitude within Earth.
com.irurueta.navigation.frames.converters	Contains converters between pairs of frames to represent position, velocity and attitude.
com.irurueta.navigation.gnss

Uses of ECEFPosition in com.irurueta.navigation.frames

Methods in com.irurueta.navigation.frames that return ECEFPosition

Modifier and Type	Method	Description
ECEFPosition	ECEFFrame.getECEFPosition()	Gets cartesian position.

Methods in com.irurueta.navigation.frames with parameters of type ECEFPosition

Modifier and Type	Method	Description
void	ECEFPosition.copyFrom(ECEFPosition input)	Copies data of provided instance into this instance.
void	ECEFPosition.copyTo(ECEFPosition output)	Copies this instance data into provided instance.
boolean	ECEFPosition.equals(ECEFPosition other)	Checks if provided instance has exactly the same contents as this instance.
boolean	ECEFPosition.equals(ECEFPosition other, double threshold)	Checks if provided instance has contents similar to this instance up to provided threshold value.
void	ECEFFrame.getECEFPosition(ECEFPosition result)	Gets cartesian position.
void	ECEFFrame.setPosition(ECEFPosition position)	Sets cartesian position.

Constructors in com.irurueta.navigation.frames with parameters of type ECEFPosition

Modifier	Constructor	Description
	ECEFFrame(ECEFPosition position)	Constructor.
	ECEFFrame(ECEFPosition position, double vx, double vy, double vz)	Constructor.
	ECEFFrame(ECEFPosition position, double vx, double vy, double vz, CoordinateTransformation c)	Constructor.
	ECEFFrame(ECEFPosition position, CoordinateTransformation c)	Constructor.
	ECEFFrame(ECEFPosition position, ECEFVelocity velocity)	Constructor.
	ECEFFrame(ECEFPosition position, ECEFVelocity velocity, CoordinateTransformation c)	Constructor.
	ECEFFrame(ECEFPosition position, com.irurueta.units.Speed speedX, com.irurueta.units.Speed speedY, com.irurueta.units.Speed speedZ)	Constructor.
	ECEFFrame(ECEFPosition position, com.irurueta.units.Speed speedX, com.irurueta.units.Speed speedY, com.irurueta.units.Speed speedZ, CoordinateTransformation c)	Constructor.
	ECEFPosition(ECEFPosition input)	Constructor.

Uses of ECEFPosition in com.irurueta.navigation.frames.converters

Methods in com.irurueta.navigation.frames.converters with parameters of type ECEFPosition

Modifier and Type	Method	Description
void	ECEFtoNEDPositionVelocityConverter.convert(ECEFPosition sourcePosition, ECEFVelocity sourceVelocity, NEDPosition destinationPosition, NEDVelocity destinationVelocity)	Converts cartesian to curvilinear position and velocity resolving axes from NED to ECEF.
void	NEDtoECEFPositionVelocityConverter.convert(double latitude, double longitude, double height, double vn, double ve, double vd, ECEFPosition destinationPosition, ECEFVelocity destinationVelocity)	Converts curvilinear to cartesian position and velocity resolving axes from NED to ECEF.
void	NEDtoECEFPositionVelocityConverter.convert(NEDPosition sourcePosition, NEDVelocity sourceVelocity, ECEFPosition destinationPosition, ECEFVelocity destinationVelocity)	Converts curvilinear to cartesian position and velocity resolving axes from NED to ECEF.
static void	ECEFtoNEDPositionVelocityConverter.convertECEFtoNED(ECEFPosition sourcePosition, ECEFVelocity sourceVelocity, NEDPosition destinationPosition, NEDVelocity destinationVelocity)	Converts cartesian to curvilinear position and velocity resolving axes from NED to ECEF.
static void	NEDtoECEFPositionVelocityConverter.convertNEDtoECEF(double latitude, double longitude, double height, double vn, double ve, double vd, ECEFPosition destinationPosition, ECEFVelocity destinationVelocity)	Converts curvilinear to cartesian position and velocity resolving axes from NED to ECEF.
static void	NEDtoECEFPositionVelocityConverter.convertNEDtoECEF(NEDPosition sourcePosition, NEDVelocity sourceVelocity, ECEFPosition destinationPosition, ECEFVelocity destinationVelocity)	Converts curvilinear to cartesian position and velocity resolving axes from NED to ECEF.

Uses of ECEFPosition in com.irurueta.navigation.gnss

Methods in com.irurueta.navigation.gnss that return ECEFPosition

Modifier and Type	Method	Description
ECEFPosition	ECEFPositionAndVelocity.getEcefPosition()	Gets ECEF position.
ECEFPosition	GNSSEstimation.getEcefPosition()	Gets estimated ECEF user position.
ECEFPosition	GNSSMeasurement.getEcefPosition()	Gets ECEF position of satellite.
ECEFPosition	GNSSConfig.getInitialEstimatedEcefPosition()	Gets initial estimated position resolved along ECEF axes.

Methods in com.irurueta.navigation.gnss with parameters of type ECEFPosition

Modifier and Type	Method	Description
private static double	GNSSBiasesGenerator.generate(ECEFPosition satellitePosition, ECEFPosition userPosition, GNSSConfig config, com.irurueta.algebra.Matrix cen, Random random)	Generates bias.
private static void	GNSSBiasesGenerator.generate(List<ECEFPosition> satellitePositions, ECEFPosition userPosition, double userLatitude, double userLongitude, GNSSConfig config, Random random, List<Double> result)	Generates biases.
static GNSSMeasurement	GNSSMeasurementsGenerator.generate(double time, ECEFPosition satellitePosition, ECEFVelocity satelliteVelocity, ECEFPosition userPosition, ECEFVelocity userVelocity, double gnssRangeErrorBias, GNSSConfig config, Random random)	Generates a single satellite GNSS measurement.
static boolean	GNSSMeasurementsGenerator.generate(double time, ECEFPosition satellitePosition, ECEFVelocity satelliteVelocity, ECEFPosition userPosition, ECEFVelocity userVelocity, double gnssRangeErrorBias, GNSSConfig config, Random random, GNSSMeasurement result)	Generates a single satellite GNSS measurement.
static Collection<GNSSMeasurement>	GNSSMeasurementsGenerator.generate(double time, List<ECEFPositionAndVelocity> satellitePositionsAndVelocities, ECEFPosition userPosition, ECEFVelocity userVelocity, List<Double> gnssRangeErrorBiases, GNSSConfig config, Random random)	Generates satellite GNSS measurements.
static void	GNSSMeasurementsGenerator.generate(double time, List<ECEFPositionAndVelocity> satellitePositionsAndVelocities, ECEFPosition userPosition, ECEFVelocity userVelocity, List<Double> gnssRangeErrorBiases, GNSSConfig config, Random random, Collection<GNSSMeasurement> result)	Generates satellite GNSS measurements.
static GNSSMeasurement	GNSSMeasurementsGenerator.generate(com.irurueta.units.Time time, ECEFPosition satellitePosition, ECEFVelocity satelliteVelocity, ECEFPosition userPosition, ECEFVelocity userVelocity, double gnssRangeErrorBias, GNSSConfig config, Random random)	Generates a single satellite GNSS measurement.
static boolean	GNSSMeasurementsGenerator.generate(com.irurueta.units.Time time, ECEFPosition satellitePosition, ECEFVelocity satelliteVelocity, ECEFPosition userPosition, ECEFVelocity userVelocity, double gnssRangeErrorBias, GNSSConfig config, Random random, GNSSMeasurement result)	Generates a single satellite GNSS measurement.
static Collection<GNSSMeasurement>	GNSSMeasurementsGenerator.generate(com.irurueta.units.Time time, List<ECEFPositionAndVelocity> satellitePositionsAndVelocities, ECEFPosition userPosition, ECEFVelocity userVelocity, List<Double> gnssRangeErrorBiases, GNSSConfig config, Random random)	Generates satellite GNSS measurements.
static void	GNSSMeasurementsGenerator.generate(com.irurueta.units.Time time, List<ECEFPositionAndVelocity> satellitePositionsAndVelocities, ECEFPosition userPosition, ECEFVelocity userVelocity, List<Double> gnssRangeErrorBiases, GNSSConfig config, Random random, Collection<GNSSMeasurement> result)	Generates satellite GNSS measurements.
static double	GNSSBiasesGenerator.generateBias(ECEFPosition satellitePosition, ECEFPosition userPosition, GNSSConfig config, Random random)	Generates biases.
static List<Double>	GNSSBiasesGenerator.generateBiases(List<ECEFPosition> satellitePositions, ECEFPosition userPosition, GNSSConfig config, Random random)	Generates biases.
static void	GNSSBiasesGenerator.generateBiases(List<ECEFPosition> satellitePositions, ECEFPosition userPosition, GNSSConfig config, Random random, List<Double> result)	Generates biases.
void	ECEFPositionAndVelocity.getEcefPosition(ECEFPosition result)	Gets ECEF position.
void	GNSSEstimation.getEcefPosition(ECEFPosition result)	Gets estimatedECEF user position.
void	GNSSMeasurement.getEcefPosition(ECEFPosition result)	Gets ECEF position of satellite.
void	GNSSConfig.getInitialEstimatedEcefPosition(ECEFPosition result)	Gets initial estimated position resolved along ECEF axes.
void	ECEFPositionAndVelocity.setEcefPosition(ECEFPosition ecefPosition)	Sets ECEF position.
void	GNSSEstimation.setEcefPosition(ECEFPosition ecefPosition)	Sets estimated ECEF user position.
void	GNSSMeasurement.setEcefPosition(ECEFPosition ecefPosition)	Sets ECEF position of satellite.
void	GNSSConfig.setInitialEstimatedEcefPosition(ECEFPosition initialEstimatedEcefPosition)	Sets initial estimated position resolved along ECEF axes.
void	GNSSConfig.setValues(double epochInterval, ECEFPosition initialEstimatedEcefPosition, int numberOfSatellites, double orbitalRadiusOfSatellites, double satellitesInclinationDegrees, double constellationLongitudeOffsetDegrees, double constellationTimingOffset, double maskAngleDegrees, double sisErrorSD, double zenithIonosphereErrorSD, double zenithTroposphereErrorSD, double codeTrackingErrorSD, double rangeRateTrackingErrorSD, double initialReceiverClockOffset, double initialReceiverClockDrift)	Sets values.
void	GNSSConfig.setValues(com.irurueta.units.Time epochInterval, ECEFPosition initialEstimatedEcefPosition, int numberOfSatellites, com.irurueta.units.Distance orbitalRadiusOfSatellites, com.irurueta.units.Angle satellitesInclination, com.irurueta.units.Angle constellationLongitudeOffset, com.irurueta.units.Time constellationTimingOffset, com.irurueta.units.Angle maskAngle, com.irurueta.units.Distance sisErrorSD, com.irurueta.units.Distance zenithIonosphereErrorSD, com.irurueta.units.Distance zenithTroposphereErrorSD, com.irurueta.units.Speed codeTrackingErrorSD, com.irurueta.units.Speed rangeRateTrackingErrorSD, com.irurueta.units.Distance initialReceiverClockOffset, com.irurueta.units.Speed initialReceiverClockDrift)	Sets values.

Method parameters in com.irurueta.navigation.gnss with type arguments of type ECEFPosition

Modifier and Type	Method	Description
private static void	GNSSBiasesGenerator.generate(List<ECEFPosition> satellitePositions, ECEFPosition userPosition, double userLatitude, double userLongitude, GNSSConfig config, Random random, List<Double> result)	Generates biases.
static List<Double>	GNSSBiasesGenerator.generateBiases(List<ECEFPosition> satellitePositions, ECEFPosition userPosition, GNSSConfig config, Random random)	Generates biases.
static void	GNSSBiasesGenerator.generateBiases(List<ECEFPosition> satellitePositions, ECEFPosition userPosition, GNSSConfig config, Random random, List<Double> result)	Generates biases.

Constructors in com.irurueta.navigation.gnss with parameters of type ECEFPosition

Modifier	Constructor	Description
	ECEFPositionAndVelocity(ECEFPosition ecefPosition)	Constructor.
	ECEFPositionAndVelocity(ECEFPosition ecefPosition, double vx, double vy, double vz)	Constructor.
	ECEFPositionAndVelocity(ECEFPosition ecefPosition, ECEFVelocity ecefVelocity)	Constructor.
	ECEFPositionAndVelocity(ECEFPosition ecefPosition, com.irurueta.units.Speed vx, com.irurueta.units.Speed vy, com.irurueta.units.Speed vz)	Constructor.
	GNSSConfig(double epochInterval, ECEFPosition initialEstimatedEcefPosition, int numberOfSatellites, double orbitalRadiusOfSatellites, double satellitesInclinationDegrees, double constellationLongitudeOffsetDegrees, double constellationTimingOffset, double maskAngleDegrees, double sisErrorSD, double zenithIonosphereErrorSD, double zenithTroposphereErrorSD, double codeTrackingErrorSD, double rangeRateTrackingErrorSD, double initialReceiverClockOffset, double initialReceiverClockDrift)	Constructor.
	GNSSConfig(com.irurueta.units.Time epochInterval, ECEFPosition initialEstimatedEcefPosition, int numberOfSatellites, com.irurueta.units.Distance orbitalRadiusOfSatellites, com.irurueta.units.Angle satellitesInclination, com.irurueta.units.Angle constellationLongitudeOffset, com.irurueta.units.Time constellationTimingOffset, com.irurueta.units.Angle maskAngle, com.irurueta.units.Distance sisErrorSD, com.irurueta.units.Distance zenithIonosphereErrorSD, com.irurueta.units.Distance zenithTroposphereErrorSD, com.irurueta.units.Speed codeTrackingErrorSD, com.irurueta.units.Speed rangeRateTrackingErrorSD, com.irurueta.units.Distance initialReceiverClockOffset, com.irurueta.units.Speed initialReceiverClockDrift)	Constructor.
	GNSSEstimation(ECEFPosition position, ECEFVelocity velocity, double clockOffset, double clockDrift)	Constructor.
	GNSSEstimation(ECEFPosition position, ECEFVelocity velocity, com.irurueta.units.Distance clockOffset, com.irurueta.units.Speed clockDrift)	Constructor.
	GNSSMeasurement(double pseudoRange, double pseudoRate, ECEFPosition position, ECEFVelocity velocity)	Constructor.
	GNSSMeasurement(com.irurueta.units.Distance pseudoRange, com.irurueta.units.Speed pseudoRate, ECEFPosition position, ECEFVelocity velocity)	Constructor.