Description

Helper method to assign a new orbit state using Mixed Spherical representation

Syntax

[Visual Basic .NET]
Public Sub AssignMixedSpherical( _ ByVal ECoordinateSystem As AgECoordinateSystem, _ ByVal Latitude As Double, _ ByVal Longitude As Double, _ ByVal Altitude As Double, _ ByVal HorFlightPathAngle As Double, _ ByVal FlightPathAzimuth As Double, _ ByVal Velocity As Double _ )

[Visual Basic .NET]

Public Sub AssignMixedSpherical( _
   ByVal ECoordinateSystem As AgECoordinateSystem, _
   ByVal Latitude As Double, _
   ByVal Longitude As Double, _
   ByVal Altitude As Double, _
   ByVal HorFlightPathAngle As Double, _
   ByVal FlightPathAzimuth As Double, _
   ByVal Velocity As Double _
)

[C#]
public void AssignMixedSpherical( AgECoordinateSystem ECoordinateSystem, double Latitude, double Longitude, double Altitude, double HorFlightPathAngle, double FlightPathAzimuth, double Velocity );

[C#]

public void AssignMixedSpherical(

   AgECoordinateSystem ECoordinateSystem, 

   double Latitude, 

   double Longitude, 

   double Altitude, 

   double HorFlightPathAngle, 

   double FlightPathAzimuth, 

   double Velocity

);

[Managed C++]
public: void AssignMixedSpherical( AgECoordinateSystem ECoordinateSystem, double Latitude, double Longitude, double Altitude, double HorFlightPathAngle, double FlightPathAzimuth, double Velocity );

[Managed C++]

public: void AssignMixedSpherical(

   AgECoordinateSystem ECoordinateSystem, 

   double Latitude, 

   double Longitude, 

   double Altitude, 

   double HorFlightPathAngle, 

   double FlightPathAzimuth, 

   double Velocity

);

[Java]
public assignMixedSpherical( AgECoordinateSystem ECoordinateSystem, double Latitude, double Longitude, double Altitude, double HorFlightPathAngle, double FlightPathAzimuth, double Velocity );

[Java]

public  assignMixedSpherical(

   AgECoordinateSystem ECoordinateSystem, 

   double Latitude, 

   double Longitude, 

   double Altitude, 

   double HorFlightPathAngle, 

   double FlightPathAzimuth, 

   double Velocity

);

[Unmanaged C++]
public: HRESULT AssignMixedSpherical( AgECoordinateSystem ECoordinateSystem, double Latitude, double Longitude, double Altitude, double HorFlightPathAngle, double FlightPathAzimuth, double Velocity );

[Unmanaged C++]

public: HRESULT AssignMixedSpherical(

   AgECoordinateSystem ECoordinateSystem, 

   double Latitude, 

   double Longitude, 

   double Altitude, 

   double HorFlightPathAngle, 

   double FlightPathAzimuth, 

   double Velocity

);

Parameters

ECoordinateSystem

Member	Value	Description
eCoordinateSystemUnknown	-1	Represents coordinate system not supported by the Object Model
eCoordinateSystemAlignmentAtEpoch	0	Alignment at Epoch: an inertial system coincident with ECF at the Coord Epoch. Often used to specify launch trajectories.
eCoordinateSystemB1950	1	B1950: X points toward the mean vernal equinox and Z points along the mean rotation axis of the Earth at the beginning of the Besselian year 1950 and corresponds to 31 December 1949 22:09:07.2 or JD 2433282.423.
eCoordinateSystemFixed	2	Fixed: X is fixed at 0 deg longitude, Y is fixed at 90 deg longitude, and Z is directed toward the north pole.
eCoordinateSystemJ2000	3	J2000: X points toward the mean vernal equinox and Z points along the mean rotation axis of the Earth on 1 Jan 2000 at 12:00:00.00 TDB, which corresponds to JD 2451545.0 TDB.
eCoordinateSystemMeanOfDate	4	Mean of Date: X points toward the mean vernal equinox and Z points along the mean rotation axis of the Earth at the Orbit Epoch.
eCoordinateSystemMeanOfEpoch	5	Mean of Epoch: X points toward the mean vernal equinox and Z points along the mean rotation axis of the Earth at the Coord Epoch.
eCoordinateSystemTEMEOfDate	6	TEME of Date: X points toward the mean vernal equinox and Z points along the true rotation axis of the Earth at the Orbit Epoch.
eCoordinateSystemTEMEOfEpoch	7	TEME of Epoch: X points toward the mean vernal equinox and Z points along the true rotation axis of the Earth at the Coord Epoch.
eCoordinateSystemTrueOfDate	8	True of Date: X points toward the true vernal equinox and Z points along the true rotation axis of the Earth at the Orbit Epoch.
eCoordinateSystemTrueOfEpoch	9	True of Epoch: X points toward the true vernal equinox and Z points along the true rotation axis of the Earth at the Coord Epoch.
eCoordinateSystemTrueOfRefDate	10	True of Ref Date: A special case of True of Epoch. Instead of the Coord Epoch, this system uses a Reference Date defined in the Integration Control page of the scenario's PODS properties.
eCoordinateSystemICRF	11	ICRF: International Celestial Reference Frame.
eCoordinateSystemMeanEarth	13	Mean Earth
eCoordinateSystemFixedNoLibration	14	uses an analytic formula not modeling lunar libration
eCoordinateSystemFixedIAU2003	15	Fixed_IAU2003
eCoordinateSystemPrincipalAxes421	16	PrincipalAxes_421
eCoordinateSystemPrincipalAxes403	17	PrincipalAxes_403
eCoordinateSystemInertial	18	Inertial
eCoordinateSystemJ2000Ecliptic	19	The mean ecliptic system evaluated at the J2000 epoch. The mean ecliptic plane is defined as the rotation of the J2000 XY plane about the J2000 X axis by the mean obliquity defined using FK5 IAU76 theory.
eCoordinateSystemTrueEclipticOfDate	21	The true ecliptic system, evaluated at each given time. The true ecliptic plane is defined as the rotation of the J2000 XY plane about the J2000 X axis by the true obliquity defined using FK5 IAU76 theory.
eCoordinateSystemPrincipalAxes430	22	PrincipalAxes_430

Latitude

Longitude

Altitude

HorFlightPathAngle

FlightPathAzimuth

Velocity

AGI STK Util 11	Send comments on this topic.
AssignMixedSpherical Method (IAgOrbitState)
See Also

Description

Syntax

Parameters

See Also