; Filename:            IBEX_2011_Orbit128InertialManeuver_5june11_v004.scr
; File type:           MAESTRO Absolute Time Sequence Script (ATS)
;
; Create time:         2011/154.171844
; Plan period start:   2011/002.000000
; Plan period stop:    2011/365.235959
; Default time format: UTC
;
; Input files:         2
;   IBEX_2011_BLANK_v001.oef
;   inertialPrecession_June_5_v002.abs
; ATS_CMD_TIME_OFFSET = 0
script ats_2011_01_02_00_00_00()
begin
  @ECT_SetHTRCmd CATBED_5N_HTR,ON $TIME=2011/06:05:08:05:00
  @ACT_SetKFInputSelect GND_CMD, 0, 0, 0, 0 $TIME=2011/06:05:08:50:00
  @ACT_SetEstUpdateEnables ENABLE, DISABLE $TIME=2011/06:05:08:50:01
  @FCT_SetFcMode burn $TIME=2011/06:05:08:57:00
  @ACT_SetInrDir 0.355813,0.637429,0.683433 $TIME=2011/06:05:08:58:00
  @ACT_SetLrTarget ACS_INERTIAL $TIME=2011/06:05:08:59:00
  @ACT_SetThrustTime 1560 $TIME=2011/06:05:08:59:55
  @ACT_SetThrustEnable ENABLE $TIME=2011/06:05:09:00:00
  @ACT_SetThrustEnable DISABLE $TIME=2011/06:05:09:25:00
  @ECT_SetHTRCmd CATBED_5N_HTR,OFF $TIME=2011/06:05:09:25:01
  @ACT_SetThrustTime 0 $TIME=2011/06:05:09:25:30
  @ACT_SetStaticZrate ESTIMATOR, 0.418 $TIME=2011/06:05:09:45:10
  @ACT_SetKFInputSelect STA_PCT_VALID, 85,18,23,90 $TIME=2011/06:05:09:45:20
  @FCT_SetFcMode Mission $TIME=2011/06:05:09:46:00
end