AGI AgAccessConstraintPlugin 11	Send comments on this topic.
Attitude Method (IAgAccessConstraintPluginObjectData)
See Also

Frame: Requested frame to express the results

Q1: Q1 component of the quaternion at the current time

Q2: Q2 component of the quaternion at the current time

Q3: Q3 component of the quaternion at the current time

Q4: Q4 component of the quaternion at the current time

Description

The attitude of the body frame of the object wrt the requested frame. Only eUtFrameInertial and eUtFrameFixed are supported.

Syntax

[Visual Basic .NET]
Public Sub Attitude( _ ByVal Frame As AgEUtFrame, _ ByRef Q1 As Double, _ ByRef Q2 As Double, _ ByRef Q3 As Double, _ ByRef Q4 As Double _ )

[Visual Basic .NET]

Public Sub Attitude( _
   ByVal Frame As AgEUtFrame, _
   ByRef Q1 As Double, _
   ByRef Q2 As Double, _
   ByRef Q3 As Double, _
   ByRef Q4 As Double _
)

[C#]
public void Attitude( AgEUtFrame Frame, ref double Q1, ref double Q2, ref double Q3, ref double Q4 );

[C#]

public void Attitude(

   AgEUtFrame Frame, 

   ref double Q1, 

   ref double Q2, 

   ref double Q3, 

   ref double Q4

);

[Managed C++]
public: void Attitude( AgEUtFrame Frame, double ^ Q1, double ^ Q2, double ^ Q3, double ^ Q4 );

[Managed C++]

public: void Attitude(

   AgEUtFrame Frame, 

   double ^ Q1, 

   double ^ Q2, 

   double ^ Q3, 

   double ^ Q4

);

[Java]
public attitude( AgEUtFrame Frame, double Q1, double Q2, double Q3, double Q4 );

[Java]

public  attitude(

   AgEUtFrame Frame, 

   double Q1, 

   double Q2, 

   double Q3, 

   double Q4

);

[Unmanaged C++]
public: HRESULT Attitude( AgEUtFrame Frame, double * Q1, double * Q2, double * Q3, double * Q4 );

[Unmanaged C++]

public: HRESULT Attitude(

   AgEUtFrame Frame, 

   double * Q1, 

   double * Q2, 

   double * Q3, 

   double * Q4

);

Parameters

Frame

Member	Value	Description
eUtFrameInertial	0
eUtFrameFixed	1
eUtFrameLVLH	2
eUtFrameNTC	3
eUtFrameICRF	4
eUtFrameJ2000	5

Requested frame to express the results

Q1

Q1 component of the quaternion at the current time

Q2

Q2 component of the quaternion at the current time

Q3

Q3 component of the quaternion at the current time

Q4

Q4 component of the quaternion at the current time

Description

Syntax

Parameters

See Also