Description
Disables the specified control parameter.
Syntax
| [Visual Basic .NET] |
|---|
Public Sub DisableControlParameter( _ ByVal Param As AgEVAControlUpdate _ ) |
| [C#] |
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public void DisableControlParameter( |
| [Managed C++] |
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public: void DisableControlParameter( |
| [Java] |
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public disableControlParameter( |
| [Unmanaged C++] |
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public: HRESULT DisableControlParameter( |
Parameters
- Param
Member Value Description eVAControlUpdateCdVal 100 Drag Coefficient (Cd) - the dimensionless drag coefficient associated with the drag area. eVAControlUpdateCrVal 101 Solar 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. eVAControlUpdateDragAreaVal 102 Drag Area - the cross-sectional area of the spacecraft assumed perpendicular to the direction of motion, used for atmospheric drag calculations. Enter a value in the selected distance unit squared. eVAControlUpdateDryMassVal 103 Dry Mass - the mass of the spacecraft exclusive of propellant. Enter a value in the selected mass unit (e.g. kg). eVAControlUpdateFuelDensityVal 104 Fuel Density - the density of the fuel tank. Enter a value in the selected mass unit per the selected distance unit cubed (e.g. kg/m^3). eVAControlUpdateFuelMassVal 105 Fuel Mass - the mass of the spacecraft propellant. Enter a value in the selected mass unit (e.g. kg). eVAControlUpdateRadiationPressureAreaVal 106 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. Enter a value in the selected distance unit squared. eVAControlUpdateRadiationPressureCoefficientVal 107 Radiation 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. eVAControlUpdateSRPAreaVal 108 Solar Radiation Pressure (Spherical) Area - the cross-sectional area of the spacecraft assumed perpendicular to the direction of solar radiation, used for solar radiation calculations. Enter a value in the selected distance unit squared. eVAControlUpdateTankPressureVal 109 Tank Pressure - the fuel tank pressure. Enter a value in the selected pressure unit (e.g. Pa). eVAControlUpdateTankTempVal 110 Tank Temperature - the temperature of the fuel tank. Enter a value in the selected temperature unit.