Description
Enables the specified control
parameter.
Syntax
| [Visual Basic .NET] |
|---|
Public Sub EnableControlParameter( _
ByVal Param As AgEVAControlManeuver _
)
|
| [C#] |
|---|
public void EnableControlParameter(
|
| [Managed C++] |
|---|
public: void EnableControlParameter(
|
| [Java] |
|---|
public enableControlParameter(
|
| [Unmanaged C++] |
|---|
public: HRESULT EnableControlParameter(
|
Parameters
- Param
-
Member Value Description eVAControlManeuverFiniteCartesianX 400 The Cartesian X component of the thrust vector. eVAControlManeuverFiniteCartesianY 401 The Cartesian Y component of the thrust vector. eVAControlManeuverFiniteCartesianZ 402 The Cartesian Z component of the thrust vector. eVAControlManeuverFiniteEulerAngles1 403 The Euler A (Phi) component of the rotation from the reference axes to the body frame. eVAControlManeuverFiniteEulerAngles2 404 The Euler B (Theta) component of the rotation from the reference axes to the body frame. eVAControlManeuverFiniteEulerAngles3 405 The Euler C (Psi) component of the rotation from the reference axes to the body frame. eVAControlManeuverFiniteSphericalAz 406 The spherical azimuth component of the thrust vector. eVAControlManeuverFiniteSphericalElev 407 The spherical elevation component of the thrust vector. eVAControlManeuverImpulsiveCartesianX 408 The Cartesian X component of the thrust vector. eVAControlManeuverImpulsiveCartesianY 409 The Cartesian Y component of the thrust vector. eVAControlManeuverImpulsiveCartesianZ 410 The Cartesian Z component of the thrust vector. eVAControlManeuverImpulsiveEulerAngles1 411 The Euler A (Phi) component of the rotation from the reference axes to the body frame. eVAControlManeuverImpulsiveEulerAngles2 412 The Euler B (Theta) component of the rotation from the reference axes to the body frame. eVAControlManeuverImpulsiveEulerAngles3 413 The Euler C (Psi) component of the rotation from the reference axes to the body frame. eVAControlManeuverImpulsiveSphericalAz 414 The spherical azimuth component of the thrust vector. eVAControlManeuverImpulsiveSphericalElev 415 The spherical elevation component of the thrust vector. eVAControlManeuverImpulsiveSphericalMag 416 The spherical magnitude component of the thrust vector. eVAControlManeuverFiniteBurnCenterBias 417 The burn center bias of the thrust. eVAControlManeuverFiniteThrustEfficiency 418 The thrust efficiency value.