######################################################
#
#NAME
# GravityBoomConfigurationForSatelliteControl.py
#
#PURPOSE:
# This is just a setup file to configure the 
# angular velocity and moment of inertia tensor to 
# simulate a gravity stabilized satellite for the 
# SatelliteControl.py script.  See that file for more 
# details.
#
######################################################

#Set up the moment of inertia tensor to be concentrated along the z axis
cxbn.InertiaTensor[0,0] = 1.000 
cxbn.InertiaTensor[0,1] = 0.000
cxbn.InertiaTensor[0,2] = 0.000
cxbn.InertiaTensor[1,0] = 0.000
cxbn.InertiaTensor[1,1] = 1.000 
cxbn.InertiaTensor[1,2] = 0.000
cxbn.InertiaTensor[2,0] = 0.000
cxbn.InertiaTensor[2,1] = 0.000
cxbn.InertiaTensor[2,2] = 0.001

#Artificially set the omega's to zero
omega.x=0 ; omega.y=0 ; omega.z=0
omega_t0=omega ; omega_t1=omega

#Use only the gravity gradient torque
UseGGTorque = 1
UseAeroTorque = 0
