Package org.orekit.propagation.analytical.gnss.data

Class NavICAlmanac

java.lang.Object

org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElementsDriversProvider

org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElements<NavICAlmanac>

org.orekit.propagation.analytical.gnss.data.CommonGnssData<NavICAlmanac>

org.orekit.propagation.analytical.gnss.data.AbstractAlmanac<NavICAlmanac>

org.orekit.propagation.analytical.gnss.data.NavICAlmanac

All Implemented Interfaces:

GNSSClockElements, TimeStamped, ParameterDriversProvider

public class NavICAlmanac
extends AbstractAlmanac<NavICAlmanac>

Class for NavIC almanac.

Since:

10.1

Author:

Bryan Cazabonne

See Also:

• "Indian Regional Navigation Satellite System, Signal In Space ICD for standard positioning service, version 1.1 - Table 28"

Field Summary

Fields inherited from class org.orekit.propagation.analytical.gnss.data.CommonGnssData

AF0, AF1, AF2

Fields inherited from class org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElements

ARGUMENT_OF_PERIGEE, ECCENTRICITY, INCLINATION, MEAN_ANOMALY, NODE_LONGITUDE, SEMI_MAJOR_AXIS

Fields inherited from class org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElementsDriversProvider

A_DOT, A_DOT_INDEX, CIC_INDEX, CIS_INDEX, CRC_INDEX, CRS_INDEX, CUC_INDEX, CUS_INDEX, DELTA_N0, DELTA_N0_DOT, DELTA_N0_DOT_INDEX, DELTA_N0_INDEX, I_DOT_INDEX, INCLINATION_COSINE, INCLINATION_RATE, INCLINATION_SINE, LATITUDE_COSINE, LATITUDE_SINE, LONGITUDE_RATE, OMEGA_DOT_INDEX, RADIUS_COSINE, RADIUS_SINE, SIZE, TIME, TIME_INDEX

Constructor Summary

Constructors

Constructor	Description
NavICAlmanac(FieldNavICAlmanac<T> original)	Constructor from field instance.
NavICAlmanac(TimeScales timeScales, SatelliteSystem system)	Constructor.

Method Summary

Modifier and Type	Method	Description
void	setSqrtA(double sqrtA)	Setter for the Square Root of Semi-Major Axis (m^1/2).
<T extends CalculusFieldElement<T>, F extends FieldGnssOrbitalElements<T, NavICAlmanac>> F	toField(Field<T> field)	Create a field version of the instance.

Methods inherited from class org.orekit.propagation.analytical.gnss.data.AbstractAlmanac

getPropagator, getPropagator

Methods inherited from class org.orekit.propagation.analytical.gnss.data.CommonGnssData

getAf0, getAf1, getAf2, getTGD, getToc, setAf0, setAf1, setAf2, setTGD, setToc

Methods inherited from class org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElements

getDate, getE, getEDriver, getI0, getI0Driver, getM0, getM0Driver, getMeanMotion0, getMu, getOmega0, getOmega0Driver, getPa, getPaDriver, getSma, getSmaDriver, setE, setGnssDate, setI0, setM0, setOmega0, setPa, setSma

Methods inherited from class org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElementsDriversProvider

copyNonKeplerian, copySelectionSettings, createDriver, getADot, getADotDriver, getAngularVelocity, getCic, getCicDriver, getCis, getCisDriver, getCrc, getCrcDriver, getCrs, getCrsDriver, getCuc, getCucDriver, getCus, getCusDriver, getCycleDuration, getDeltaN0, getDeltaN0Dot, getDeltaN0DotDriver, getDeltaN0Driver, getIDot, getIDotDriver, getOmegaDot, getOmegaDotDriver, getParametersDrivers, getPRN, getSystem, getTime, getTimeDriver, getTimeScales, getWeek, getWeeksInCycle, isCivilianMessage, setADot, setCic, setCis, setCrc, setCrs, setCuc, setCus, setDeltaN0, setDeltaN0Dot, setIDot, setOmegaDot, setPRN, setTime, setWeek

Methods inherited from class java.lang.Object

clone, equals, finalize, getClass, hashCode, notify, notifyAll, toString, wait, wait, wait

Methods inherited from interface org.orekit.utils.ParameterDriversProvider

getNbParametersDriversValue, getParameterDriver, getParameters, getParameters, getParameters, getParameters, getParametersAllValues, getParametersAllValues, isSupported

Methods inherited from interface org.orekit.time.TimeStamped

durationFrom, getDate

Constructor Details

NavICAlmanac

public NavICAlmanac(TimeScales timeScales,
 SatelliteSystem system)

Constructor.

Parameters:

timeScales - known time scales

system - satellite system to consider for interpreting week number (may be different from real system, for example in Rinex nav, weeks are always according to GPS)

NavICAlmanac

public NavICAlmanac(FieldNavICAlmanac<T> original)

Constructor from field instance.

Type Parameters:

T - type of the field elements

Parameters:

original - regular field instance

Method Details

toField

public <T extends CalculusFieldElement<T>,
F extends FieldGnssOrbitalElements<T,
NavICAlmanac>>
F toField(Field<T> field)

Create a field version of the instance.

Specified by:

toField in class GNSSOrbitalElements<NavICAlmanac>

Type Parameters:

T - type of the field elements

F - type of the orbital elements (field version)

Parameters:

field - field to which elements belong

Returns:

field version of the instance

setSqrtA

public void setSqrtA(double sqrtA)

Setter for the Square Root of Semi-Major Axis (m^1/2).

In addition, this method set the value of the Semi-Major Axis.

Parameters:

sqrtA - the Square Root of Semi-Major Axis (m^1/2)