# SIMULATORCONTROLLER ## START TIME startTime.year=2017 startTime.month=6 startTime.day=1 startTime.hour=0 startTime.minute=0 startTime.second=0 ## ORBIT PARAMETERS # a - semi-major axis (km), negative for hyperbolic orbits orbit.a=7130.092d # e - eccentricity orbit.e=0.001111d # i - inclination (deg) orbit.i=98.405d # pa - perigee argument (deg) orbit.pa=98.405d # raan - right ascension of ascending node (deg) orbit.raan=227.088d # mean - anomaly mean anomaly (rad) orbit.mean=305d ## INITIAL CONDITION initial.eulerangle.x=0 initial.eulerangle.y=0 initial.eulerangle.z=180 initial.angularVelocity.x=0 initial.angularVelocity.y=0 initial.angularVelocity.z=0.024d ## SIMULATION CONFIGURATION # simulation time in seconds simulation.time=700d # simulation step in seconds simulation.step=.01d # how many points to store to plt the graphs simulation.intervalToStore=2000 # reaction wheel controller name simulation.reactionWheelControllerName=ProportionalNonLinearQuaternionSDREController_GIBBS # magnetorquer controller name #simulation.magnetorquersController=SetOfMagnetorquersController # SATELLITE satellite.properties=amazonia1