CCSDS_ACM_VERS = 2.0

CREATION_DATE            = 2017-12-01T00:00:00
ORIGINATOR               = NASA
MESSAGE_ID               = A7015Z5

META_START
OBJECT_NAME              = SDO
INTERNATIONAL_DESIGNATOR = 2010-005A
TIME_SYSTEM              = UTC
EPOCH_TZERO              = 2017-12-26T19:40:00.000
META_STOP

ATT_START
COMMENT                   OBC Attitude and Bias during momentum management maneuver
REF_FRAME_A              = J2000
REF_FRAME_B              = SC_BODY_1
NUMBER_STATES            = 7
ATT_TYPE                 = QUATERNION
RATE_TYPE                = GYRO_BIAS
  0.000000 0.1153 -0.1424 0.8704 0.4571 2.271e-06 -4.405e-06 -3.785e-06
  2.000000 0.1153 -0.1424 0.8704 0.4571 2.271e-06 -4.405e-06 -3.785e-06
 99.80183  0.1017 -0.1332 0.8806 0.4433 2.587e-06  8.769e-06  5.436e-06
599.80275  0.1152 -0.1423 0.8704 0.4571 2.48e-06  -4.350e-06 -3.779e-06
ATT_STOP

MAN_START
COMMENT                    Momentum management maneuver
MAN_PURPOSE              = MOM_DESAT
MAN_BEGIN_TIME           = 100.0
MAN_DURATION             = 450.0
ACTUATOR_USED            = ATT-THRUSTER
TARGET_MOMENTUM          = 1.30 -16.400 -11.350
TARGET_MOM_FRAME         = EME2000
MAN_STOP

AD_START
COMMENT                    SDO Onboard Filter
AD_METHOD                = EKF
ATTITUDE_SOURCE          = OBC
ATTITUDE_STATES          = QUATERNION
REF_FRAME_A              = J2000
REF_FRAME_B              = SC_BODY_1
SENSOR_START
SENSOR_NUMBER            = 1
SENSOR_USED              = AST1
SENSOR_STOP
SENSOR_START
SENSOR_NUMBER            = 2
SENSOR_USED              = AST2
SENSOR_STOP
SENSOR_START
SENSOR_NUMBER            = 3
SENSOR_USED              = DSS
SENSOR_STOP
SENSOR_START
SENSOR_NUMBER            = 4
SENSOR_USED              = IMU
SENSOR_STOP
AD_STOP
