Disables the specified control
parameter.
| [Visual Basic .NET] |
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Public Sub DisableControlParameter( _
ByVal Param As AgEVAControlThrusters _
)
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| [C#] |
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public void DisableControlParameter(
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| [Managed C++] |
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public: void DisableControlParameter(
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| [Java] |
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public disableControlParameter(
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| [Unmanaged C++] |
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public: HRESULT DisableControlParameter(
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- 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.