Description
Sets the attitude control type.
Syntax
| [Visual Basic .NET] |
|---|
Public Sub SetAttitudeControlType( _ ByVal AttitudeControlType As AgEVAAttitudeControl _ ) |
| [C#] |
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public void SetAttitudeControlType( |
| [Managed C++] |
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public: void SetAttitudeControlType( |
| [Java] |
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public setAttitudeControlType( |
| [Unmanaged C++] |
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public: HRESULT SetAttitudeControlType( |
Parameters
- AttitudeControlType
Member Value Description eVAAttitudeControlVelocityVector 0 Along Velocity Vector - attitude is such that the total thrust vector is aligned with the spacecraft's inertial velocity vector. eVAAttitudeControlAntiVelocityVector 1 Anti-Velocity Vector - attitude is such that the total thrust vector is opposite to the spacecraft's inertial velocity vector. eVAAttitudeControlAttitude 2 Attitude - attitude is defined using Euler Angles or a Quaternion. eVAAttitudeControlFile 3 File - import an attitude file to set the maneuver. eVAAttitudeControlThrustVector 4 Thrust Vector - the total thrust vector can be specified in cartesian or spherical form with respect to the thrust axes. eVAAttitudeControlPlugin 5 Plugin - attitude is defined using a COM plugin. eVAAttitudeControlTimeVarying 6 Time Varying - polynomial and sine representations for the azimuth and elevation of the thrust vector.