Description
Sets the attitude control type.
Syntax
| [Visual Basic .NET] |
|---|
Public Sub SetAttitudeControlType( _
ByVal AttitudeControlType As AgEVAAttitudeControl _
)
|
| [C#] |
|---|
public void SetAttitudeControlType(
|
| [Managed C++] |
|---|
public: void SetAttitudeControlType(
|
| [Java] |
|---|
public setAttitudeControlType(
|
| [Unmanaged C++] |
|---|
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.