AGI STK Astrogator 11Send comments on this topic.
SetActionAndValue Method (IAgVAMCSUpdate)
See Also 
ParameterType
ActionType
Value
Windows






Windows & Linux

Description

Sets an action and the new value.

Syntax

[Visual Basic .NET]
Public Sub SetActionAndValue( _
   ByVal ParameterType As AgEVAUpdateParam, _
   ByVal ActionType As AgEVAUpdateAction, _
   ByVal Value As Double _
) 
[C#]
public void SetActionAndValue(
   AgEVAUpdateParam ParameterType,
   AgEVAUpdateAction ActionType,
   double Value
);
[Managed C++]
public: void SetActionAndValue(
   AgEVAUpdateParam ParameterType,
   AgEVAUpdateAction ActionType,
   double Value
);
[Java]
public  setActionAndValue(
   AgEVAUpdateParam ParameterType,
   AgEVAUpdateAction ActionType,
   double Value
);
[Unmanaged C++]
public: HRESULT SetActionAndValue(
   AgEVAUpdateParam ParameterType,
   AgEVAUpdateAction ActionType,
   double Value
);

Parameters

ParameterType
MemberValueDescription
eVAUpdateParamDragArea0Drag Area - the cross-sectional area of the spacecraft assumed perpendicular to the direction of motion, used for atmospheric drag calculations.
eVAUpdateParamSRPArea1Solar Radiation Pressure (Spherical) Area - the cross-sectional area of the spacecraft assumed perpendicular to the direction of solar radiation, used for solar radiation calculations.
eVAUpdateParamDryMass2Dry Mass - the mass of the spacecraft exclusive of propellant.
eVAUpdateParamFuelMass3The mass of the spacecraft propellant.
eVAUpdateParamFuelDensity4The density of the fuel tank.
eVAUpdateParamTankPressure5The fuel tank pressure.
eVAUpdateParamTankTemp6The temperature of the fuel tank.
eVAUpdateParamCr7Solar Radiation Pressure (Spherical) Coefficient (Cr) - the reflectivity of the spacecraft used for solar radiation pressure calculations, where 2.0 is fully reflective and 1.0 is not reflective at all.
eVAUpdateParamCd8Drag Coefficient (Cd) - the dimensionless drag coefficient associated with the drag area.
eVAUpdateParamCk9Radiation Pressure (Albedo/Thermal) Coefficient (Ck) - the reflectivity of the spacecraft used for central body radiation pressure (albedo / thermal pressure) calculations, where 2.0 is fully reflective and 1.0 is not reflective at all.
eVAUpdateParamRadiationPressureArea10Radiation Pressure (Albedo/Thermal) Area - the cross-sectional area of the spacecraft assumed perpendicular to the direction of central body radiation, used for central body radiation (albedo / thermal pressure) calculations.
ActionType
MemberValueDescription
eVAUpdateActionNoChange0No change in value - leave the current value for this parameter unchanged (ignoring any quantity that may appear in the Value column).
eVAUpdateActionAddValue1Add value - add the quantity entered in the Value column to the current value for this parameter.
eVAUpdateActionSubtractValue2Subtract value - subtract the quantity entered in the Value column from the current value for this parameter.
eVAUpdateActionSetToNewValue3Set to new value - replace the current value for this parameter with the quantity entered in the Value column.
Value

See Also

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