Description
Enables the specified control parameter.
Syntax
| [Visual Basic .NET] |
|---|
Public Sub EnableControlParameter( _ ByVal Param As AgEVAControlManeuver _ ) |
| [C#] |
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public void EnableControlParameter( |
| [Managed C++] |
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public: void EnableControlParameter( |
| [Java] |
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public enableControlParameter( |
| [Unmanaged C++] |
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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. eVAControlManeuverFiniteAz0 419 The time varying azimuth polynomial constant term. eVAControlManeuverFiniteAz1 420 The time varying azimuth polynomial linear term. eVAControlManeuverFiniteAz2 421 The time varying azimuth polynomial quadratic term. eVAControlManeuverFiniteAz3 422 The time varying azimuth polynomial cubic term. eVAControlManeuverFiniteAz4 423 The time varying azimuth polynomial quartic term. eVAControlManeuverFiniteAzA 424 The time varying azimuth sine amplitude term. eVAControlManeuverFiniteAzF 425 The time varying azimuth sine frequency term. eVAControlManeuverFiniteAzP 426 The time varying azimuth sine phase term. eVAControlManeuverFiniteEl0 427 The time varying elevation polynomial constant term. eVAControlManeuverFiniteEl1 428 The time varying elevation polynomial linear term. eVAControlManeuverFiniteEl2 429 The time varying elevation polynomial quadratic term. eVAControlManeuverFiniteEl3 430 The time varying elevation polynomial cubic term. eVAControlManeuverFiniteEl4 431 The time varying elevation polynomial quartic term. eVAControlManeuverFiniteElA 432 The time varying elevation sine amplitude term. eVAControlManeuverFiniteElF 433 The time varying elevation sine frequency term. eVAControlManeuverFiniteElP 434 The time varying elevation sine phase term.