Description
Converts the from3Vector from the fromAttitude reference system to the toAttitude reference system, using referenceGroundVehicle as the reference GroundVehicle.
Timing Precision Mode
This page describes functionality in nanosecond timing precision mode.
Function Signature
Arguments
fromAttitude


Description:

Attitude system of input state.

Valid Values:

Value

Label

0

Mean of J2000 inertial reference system

8

GroundVehicles's current velocitylocal tangent (VLT) reference system

9

GroundVehicles's current EarthNorthUp (ENU) reference system


toAttitude


Description:

Attitude system of output state.

Valid Values:

Value

Label

0

Mean of J2000 inertial reference system

8

GroundVehicles's current velocitylocal tangent (VLT) reference system

9

GroundVehicles's current EarthNorthUp (ENU) reference system


referenceGroundVehicle


Description:

The GroundVehicle object to which the attitude frames are referenced.

from3Vector


Description:

A threeelement array containing the position vector in the input attitude system.

Required Size:

At least 3

Return Value
Type:

Array of number (size = 3)

Returns a threeelement array containing the converted vector in the output attitude system.
Syntax
myArray1 = AttitudeConvert(myVariable1, myVariable2, myGroundVehicle1, myArray2);

See also
AttitudeConvert
