Description
Enables the specified control
parameter.
Syntax
| [Visual Basic .NET] |
|---|
Public Sub EnableControlParameter( _
ByVal Param As AgEVAControlThrusters _
)
|
| [C#] |
|---|
public void EnableControlParameter(
|
| [Managed C++] |
|---|
public: void EnableControlParameter(
|
| [Java] |
|---|
public enableControlParameter(
|
| [Unmanaged C++] |
|---|
public: HRESULT EnableControlParameter(
|
Parameters
- Param
-
Member Value Description eVAControlThrustersEquivOnTime 0 The equivalent on-time percentage is a factor multiplied by the thrust. The thrust is applied continuously throughout the maneuver and is reduced by the percentage. The mass flow rate is likewise reduced. E.g., for an on-time percentage of 75, the acceleration on the spacecraft will be reduced by 25, and only 75% of the fuel will be used. eVAControlThrustersThrustEfficiency 1 The thruster efficiency. eVAControlThrustersSphericalAzimuth 2 Thruster direction defined as a vector in the body frame. Spherical azimuth value. eVAControlThrustersSphericalElevation 3 Thruster direction defined as a vector in the body frame. Spherical elevation value. eVAControlThrustersCartesianX 4 Thruster direction defined as a vector in the body frame. Cartesian X value. eVAControlThrustersCartesianY 5 Thruster direction defined as a vector in the body frame. Cartesian Y value. eVAControlThrustersCartesianZ 6 Thruster direction defined as a vector in the body frame. Cartesian Z value.