Class BaselineCalculation

Baseline calculation helper class.

Inheritance
System.Object
BaselineCalculation
Namespace: Stac.Extensions.Sat
Assembly: DotNetStac.dll
Syntax
public class BaselineCalculation : object

Methods

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Ax(Double, IInterpolation[])

Calculates the orbit value.

Declaration
public static double Ax(double time, IInterpolation[] orbitStates)
Parameters
Type Name Description
System.Double time

Time.
IInterpolation[] orbitStates

Orbit states.
Returns
Type Description
System.Double

The orbit value.
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Ay(Double, IInterpolation[])

Calculates the orbit value.

Declaration
public static double Ay(double time, IInterpolation[] orbitStates)
Parameters
Type Name Description
System.Double time

Time.
IInterpolation[] orbitStates

Orbit states.
Returns
Type Description
System.Double

The orbit value.
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Az(Double, IInterpolation[])

Calculates the orbit value.

Declaration
public static double Az(double time, IInterpolation[] orbitStates)
Parameters
Type Name Description
System.Double time

Time.
IInterpolation[] orbitStates

Orbit states.
Returns
Type Description
System.Double

The orbit value.
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CalculateBaseline(DateTime[], SatOrbitStateVector[], SatOrbitStateVector[], IPosition)

Calculates the baseline.

Declaration
public static BaselineVector CalculateBaseline(DateTime[] time, SatOrbitStateVector[] master, SatOrbitStateVector[] slave, IPosition groundPoint)
Parameters
Type Name Description
DateTime[] time

Time.
SatOrbitStateVector[] master

Master.
SatOrbitStateVector[] slave

Slave.
IPosition groundPoint

Ground point.
Returns
Type Description
BaselineVector

The baseline.
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PolyInterpol(DateTime, SatOrbitStateVector[])

Interpolates the orbit state vectors.

Declaration
public static IInterpolation[] PolyInterpol(DateTime time0, SatOrbitStateVector[] orbitStateVectors)
Parameters
Type Name Description
DateTime time0

Time of the orbit state vector to interpolate
SatOrbitStateVector[] orbitStateVectors

The orbit state vectors.
Returns
Type Description
IInterpolation[]

Interpolated orbit state vectors.
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Sx(Double, IInterpolation[])

Calculates the orbit value.

Declaration
public static double Sx(double time, IInterpolation[] orbitStates)
Parameters
Type Name Description
System.Double time

Time.
IInterpolation[] orbitStates

Orbit states.
Returns
Type Description
System.Double

The orbit value.
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Sy(Double, IInterpolation[])

Calculates the orbit value.

Declaration
public static double Sy(double time, IInterpolation[] orbitStates)
Parameters
Type Name Description
System.Double time

Time.
IInterpolation[] orbitStates

Orbit states.
Returns
Type Description
System.Double

The orbit value.
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SynchronizeVector(Double, IPosition, IInterpolation[], out Boolean, out Double, Int32, Double)

Synchronizes the vector.

Declaration
public static double SynchronizeVector(double t0, IPosition groundPoint, IInterpolation[] slave, out bool converged, out double maxError, int maxIterations = 100, double tolerance = 1E-08)
Parameters
Type Name Description
System.Double t0

T0.
IPosition groundPoint

Ground point.
IInterpolation[] slave

Slave.
System.Boolean converged

Converged.
System.Double maxError

Max error.
System.Int32 maxIterations

Max iterations.
System.Double tolerance

Tolerance.
Returns
Type Description
System.Double

The vector.
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SynchronizeVector2(Double, IPosition, IInterpolation[], out Boolean, out Double, Int32, Double)

Synchronizes the vector2.

Declaration
public static double SynchronizeVector2(double t0, IPosition groundPoint, IInterpolation[] interpol, out bool converged, out double maxError, int maxIterations = 100, double tolerance = 1E-08)
Parameters
Type Name Description
System.Double t0

T0.
IPosition groundPoint

Ground point.
IInterpolation[] interpol

Interpol.
System.Boolean converged

Converged.
System.Double maxError

Max error.
System.Int32 maxIterations

Max iterations.
System.Double tolerance

Tolerance.
Returns
Type Description
System.Double

The vector2.
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Sz(Double, IInterpolation[])

Calculates the orbit value.

Declaration
public static double Sz(double time, IInterpolation[] orbitStates)
Parameters
Type Name Description
System.Double time

Time.
IInterpolation[] orbitStates

Orbit states.
Returns
Type Description
System.Double

The orbit value.
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VectorProduct3D(Double[], Double[])

Calculates 3D vector product

Declaration
public static double[] VectorProduct3D(double[] vectorA, double[] vectorB)
Parameters
Type Name Description
System.Double[] vectorA

Vector A.
System.Double[] vectorB

Vector B.
Returns
Type Description
System.Double[]

3D vector product.
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Vx(Double, IInterpolation[])

Calculates the orbit value.

Declaration
public static double Vx(double time, IInterpolation[] orbitStates)
Parameters
Type Name Description
System.Double time

Time.
IInterpolation[] orbitStates

Orbit states.
Returns
Type Description
System.Double

The orbit value.
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Vy(Double, IInterpolation[])

Calculates the orbit value.

Declaration
public static double Vy(double time, IInterpolation[] orbitStates)
Parameters
Type Name Description
System.Double time

Time.
IInterpolation[] orbitStates

Orbit states.
Returns
Type Description
System.Double

The orbit value.
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Vz(Double, IInterpolation[])

Calculates the orbit value.

Declaration
public static double Vz(double time, IInterpolation[] orbitStates)
Parameters
Type Name Description
System.Double time

Time.
IInterpolation[] orbitStates

Orbit states.
Returns
Type Description
System.Double

The orbit value.

Extension Methods