<T extends CalculusFieldElement<T>> T |
EstimatedIonosphericModel.pathDelay(FieldSpacecraftState<T> state,
TopocentricFrame baseFrame,
double frequency,
T[] parameters) |
Calculates the ionospheric path delay for the signal path from a ground
station to a satellite.
|
double |
EstimatedIonosphericModel.pathDelay(SpacecraftState state,
TopocentricFrame baseFrame,
double frequency,
double[] parameters) |
Calculates the ionospheric path delay for the signal path from a ground
station to a satellite.
|
<T extends CalculusFieldElement<T>> T |
GlobalIonosphereMapModel.pathDelay(FieldSpacecraftState<T> state,
TopocentricFrame baseFrame,
double frequency,
T[] parameters) |
|
double |
GlobalIonosphereMapModel.pathDelay(SpacecraftState state,
TopocentricFrame baseFrame,
double frequency,
double[] parameters) |
|
<T extends CalculusFieldElement<T>> T |
IonosphericModel.pathDelay(FieldSpacecraftState<T> state,
TopocentricFrame baseFrame,
double frequency,
T[] parameters) |
Calculates the ionospheric path delay for the signal path from a ground
station to a satellite.
|
double |
IonosphericModel.pathDelay(SpacecraftState state,
TopocentricFrame baseFrame,
double frequency,
double[] parameters) |
Calculates the ionospheric path delay for the signal path from a ground
station to a satellite.
|
<T extends CalculusFieldElement<T>> T |
KlobucharIonoModel.pathDelay(FieldSpacecraftState<T> state,
TopocentricFrame baseFrame,
double frequency,
T[] parameters) |
Calculates the ionospheric path delay for the signal path from a ground
station to a satellite.
|
double |
KlobucharIonoModel.pathDelay(SpacecraftState state,
TopocentricFrame baseFrame,
double frequency,
double[] parameters) |
Calculates the ionospheric path delay for the signal path from a ground
station to a satellite.
|
<T extends CalculusFieldElement<T>> T |
NeQuickModel.pathDelay(FieldSpacecraftState<T> state,
TopocentricFrame baseFrame,
double frequency,
T[] parameters) |
|
double |
NeQuickModel.pathDelay(SpacecraftState state,
TopocentricFrame baseFrame,
double frequency,
double[] parameters) |
|
<T extends CalculusFieldElement<T>> T |
PythonIonosphericModel.pathDelay(FieldSpacecraftState<T> state,
TopocentricFrame baseFrame,
double frequency,
T[] parameters) |
Calculates the ionospheric path delay for the signal path from a ground
station to a satellite.
|
double |
PythonIonosphericModel.pathDelay(SpacecraftState state,
TopocentricFrame baseFrame,
double frequency,
double[] parameters) |
Calculates the ionospheric path delay for the signal path from a ground
station to a satellite.
|
<T extends CalculusFieldElement<T>> T |
SsrVtecIonosphericModel.pathDelay(FieldSpacecraftState<T> state,
TopocentricFrame baseFrame,
double frequency,
T[] parameters) |
Calculates the ionospheric path delay for the signal path from a ground
station to a satellite.
|
double |
SsrVtecIonosphericModel.pathDelay(SpacecraftState state,
TopocentricFrame baseFrame,
double frequency,
double[] parameters) |
Calculates the ionospheric path delay for the signal path from a ground
station to a satellite.
|
<T extends CalculusFieldElement<T>> T |
PythonIonosphericModel.pathDelay_FTdT(FieldSpacecraftState<T> state,
TopocentricFrame baseFrame,
double frequency,
T[] parameters) |
|
double |
PythonIonosphericModel.pathDelay_STdd(SpacecraftState state,
TopocentricFrame baseFrame,
double frequency,
double[] parameters) |
|