Description
Enables the specified control
parameter.
Syntax
| [Visual Basic .NET] |
|---|
Public Sub EnableControlParameter( _
ByVal Param As AgEVAControlFollow _
)
|
| [C#] |
|---|
public void EnableControlParameter(
|
| [Managed C++] |
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public: void EnableControlParameter(
|
| [Java] |
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public enableControlParameter(
|
| [Unmanaged C++] |
|---|
public: HRESULT EnableControlParameter(
|
Parameters
- Param
-
Member Value Description eVAControlFollowFuelMass 200 Fuel Mass - the mass of the spacecraft propellant. Enter a value in the selected mass unit (e.g. kg). eVAControlFollowCd 201 Drag Coefficient (Cd) - the dimensionless drag coefficient associated with the drag area. eVAControlFollowCr 202 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. eVAControlFollowDragArea 203 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. eVAControlFollowDryMass 204 Dry Mass - the mass of the spacecraft exclusive of propellant. Enter a value in the selected mass unit (e.g. kg). eVAControlFollowFuelDensity 205 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). eVAControlFollowK1 206 GPS Solar Radiation Pressure K1 - if you are using a non-spherical SRP model, this field defines the model's K1 (scale) value. eVAControlFollowK2 207 GPS Solar Radiation Pressure K2 - if you are using a non-spherical SRP model, this field defines the model's K2 (Y bias) value. eVAControlFollowRadiationPressureArea 208 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. eVAControlFollowCk 209 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. eVAControlFollowSRPArea 210 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. eVAControlFollowTankPressure 211 Tank Pressure - the fuel tank pressure. Enter a value in the selected pressure unit (e.g. Pa). eVAControlFollowTankTemp 212 Tank Temperature - the temperature of the fuel tank. Enter a value in the selected temperature unit. eVAControlFollowMaxFuelMass 213 Maximum Fuel Mass - the maximum fuel mass of the spacecraft; this parameter specifically applies to Finite Maneuver segments that are being executed in Backward Sequences. Enter a value in the selected mass unit (e.g. kg). eVAControlFollowTankVolume 214 Tank Volume - the volume of the fuel tank. Enter a value in the selected distance unit cubed (e.g. m^3). The minimum value is 1e-019 m^3. eVAControlFollowXOffset 215 X Offset - the distance that the spacecraft will be offset from the leader's body frame along the X axis. eVAControlFollowYOffset 216 Y Offset - the distance that the spacecraft will be offset from the leader's body frame along the Y axis. eVAControlFollowZOffset 217 Z Offset - the distance that the spacecraft will be offset from the leader's body frame along the Z axis.