AddAttitude EulerRates
Adds attitude data based on a time-ordered set of Euler angle rates.
Syntax
AddAttitude <ObjectPath> EulerRates {StartTime} {Sequence} <AngleRate1> <AngleRate2> <AngleRate3>
Description
Use the AddAttitude EulerRates command to modify the attitude of a vehicle using rates of Euler angles attitude data.
The {Sequence} parameter identifies the order of rotations for converting the Euler angles to a quaternion. Valid values for {Sequence} are 121, 123, 131, 132, 212, 213, 231, 232, 312, 313, 321, 323.
The angle rate values, <AngleRate1> <AngleRate2> <AngleRate3>, are entered in degrees/second.
For valid {StartTime} values see Time Options.
The AddAttitude EulerRates command is similar to using an external attitude profile, except that the points are entered one at a time using this command.
At least one attitude data point must be added before using the AddAttitude EulerRates command, otherwise the command will NACK.
Multiple inputs of attitude data must be entered with increasing times. If you attempt to enter attitude data that is dated prior to existing attitude data, the new entry is ignored. To clear old data, use the SetAttitude ClearData command.
Examples
The following commands will add three points to Satellite1's attitude:
Return message
Group membership
This command belongs to the following group(s):
Version
10