[Isocops] IBEX Orbit# 177 ATS v001 (22 Aug 12 - 31 Aug 12)

Wed Aug 8 18:30:51 EDT 2012

Guys,
    I have attached V002 of the Orbit# 177 ATS.  The V002 ATS includes
battery balancing commands during PERIGEE.
The commands begin 30 minutes before PERIGEE and end 1 1/2 hrs before the
0900 UTC contact
I will place the new ATS on the SFTP before tomorrow morning

On Wed, Aug 8, 2012 at 8:00 AM, Ibex Mission Operations
<ibexops at gmail.com>wrote:

> Guys,
> Here are the planning files for Orbit# 177.
> *All comments/approvals are due before 10 Aug 12 @1800 UTC*
> *
> *Please note the following:
> 1. Sun Precession Maneuver at Perigee
> 2012-08-30T17:07:13.175Z,StarTrackerOutageStart,orbit:177,dueTo:overlap
> 2012-08-31T12:14:00.000Z,StarTrackerOutageStop,orbit:177,dueTo:overlap
> 2. No contact commands due to limited stored command space.
> All contacts will be treated as Blind_Acq contacts
> 3. No battery balancing commands due to possible  Special OPS at Perigee
>
>
>
>
>
> --
> Sheral R. Wesley
> SPVR., Satellite Operations
> IBEX Mission OPS
> (304) 279-6678
>

-- 
Sheral R. Wesley
SPVR., Satellite Operations
IBEX Mission OPS
(304) 279-6678
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; Filename:            IBEX_2012_235_o0177a_v002.scr
; File type:           MAESTRO Absolute Time Sequence Script (ATS)
;
; Create time:         2012/220.201404
; Plan period start:   2012/235.081400
; Plan period stop:    2012/244.121300
; Default time format: UTC
;
; Input files:         4
;   IBEX_2012_235_o0177a_v001.oef
;   IBEX_2012_234_o0177a_v002.stf
;   IBEX_2012_forecast_07aug12-21sep12_v001.sap
;   IBEX_2011_Orbit177_v001.caf
; ATS_CMD_TIME_OFFSET = 0
script ats_2012_08_22_08_14_00()
begin
#  Orbit# 177 Ascending BUS Commands
  @ACT_SetSpinPulseProtectEnable Disable $TIME=2012/08:22:08:16:18
  @FCT_SetScState science $TIME=2012/08:22:08:16:20
  @ACT_SetSpinPulseProtectEnable Enable $TIME=2012/08:22:08:16:22
  @CEU_LO_SCIENCE_MODE NORMAL $TIME=2012/08:22:08:16:24

#  ORbit# 177 Ascending Payload Commands  
  @CEU_MACRO_EXEC ASCENDING_PL1 $TIME=2012/08:22:14:38:06
  @CEU_MACRO_EXEC ASCENDING_HI $TIME=2012/08:22:14:38:22
  @CEU_SET_PARAMETER 1, TLM_RATE_SOH $TIME=2012/08:22:14:49:16
  @CEU_SET_PARAMETER 4, HV_STEP_DWELL $TIME=2012/08:22:14:49:19
  @CEU_SET_PARAMETER 3, HV_STEP_FRAC $TIME=2012/08:22:14:49:23
  @CEU_HI_CEM_4_LVL 1800 $TIME=2012/08:22:14:49:27
  @CEU_SET_PARAMETER 0, TLM_RATE_SOH $TIME=2012/08:22:14:49:44
  @CEU_MACRO_EXEC ASCENDING_PL2 $TIME=2012/08:22:14:49:47

#  Orbit# 177 APOGEE: Descending Payload Commands 
  @CEU_MACRO_EXEC DESCENDING_PL1 $TIME=2012/08:26:05:06:39
  @CEU_MACRO_EXEC DESCENDING_HI $TIME=2012/08:26:05:07:21
  @CEU_MACRO_EXEC DESCENDING_PL2 $TIME=2012/08:26:05:17:40

#  Orbit# 177 APOGEE: Inertial MAneuver Commands  
  @FCT_SetScState housekeeping $TIME=2012/08:26:05:51:30
  @ECT_SetHTRCmd CATBED_5N_HTR,ON $TIME=2012/08:26:05:56:28
  @ACT_SetKFInputSelect GND_CMD, 0, 0, 0, 0 $TIME=2012/08:26:06:41:28
  @ACT_SetEstUpdateEnables ENABLE, DISABLE $TIME=2012/08:26:06:41:29
  @FCT_SetFcMode burn $TIME=2012/08:26:06:48:28
  @ACT_SetInrDir -0.877199,0.445336,0.179438 $TIME=2012/08:26:06:49:28
  @ACT_SetLrTarget ACS_INERTIAL $TIME=2012/08:26:06:50:28
  @ACT_SetThrustTime 660 $TIME=2012/08:26:06:51:23
  @ACT_SetThrustEnable ENABLE $TIME=2012/08:26:06:51:28
  @ACT_SetThrustEnable DISABLE $TIME=2012/08:26:07:01:28
  @ECT_SetHTRCmd CATBED_5N_HTR,OFF $TIME=2012/08:26:07:01:29
  @ACT_SetThrustTime 0 $TIME=2012/08:26:07:01:58
  @ACT_SetStaticZrate ESTIMATOR, 0.418 $TIME=2012/08:26:07:16:38
  @ACT_SetKFInputSelect STA_PCT_VALID, 48,18,23,53 $TIME=2012/08:26:07:16:48
  @FCT_SetFcMode Mission $TIME=2012/08:26:07:17:28

#  Orbit# 177 APOGEE: Ascending BUS Commands  
  @ACT_SetSpinPulseProtectEnable Disable $TIME=2012/08:26:08:06:34
  @FCT_SetScState science $TIME=2012/08:26:08:06:36
  @ACT_SetSpinPulseProtectEnable Enable $TIME=2012/08:26:08:06:38
  @CEU_LO_SCIENCE_MODE NORMAL $TIME=2012/08:26:08:06:40

#  Orbit# 177 APOGEE: Ascending Payload Commands  
  @CEU_MACRO_EXEC ASCENDING_PL1 $TIME=2012/08:26:08:36:34
  @CEU_MACRO_EXEC ASCENDING_HI $TIME=2012/08:26:08:36:50
  @CEU_SET_PARAMETER 1, TLM_RATE_SOH $TIME=2012/08:26:08:47:44
  @CEU_SET_PARAMETER 4, HV_STEP_DWELL $TIME=2012/08:26:08:47:47
  @CEU_SET_PARAMETER 3, HV_STEP_FRAC $TIME=2012/08:26:08:47:51
  @CEU_HI_CEM_4_LVL 1800 $TIME=2012/08:26:08:47:55
  @CEU_SET_PARAMETER 0, TLM_RATE_SOH $TIME=2012/08:26:08:48:12
  @CEU_MACRO_EXEC ASCENDING_PL2 $TIME=2012/08:26:08:48:15

#  Orbit# 177 PERIGEE: Descending Payload Commands  
  @CEU_MACRO_EXEC DESCENDING_PL1 $TIME=2012/08:30:18:34:28
  @CEU_MACRO_EXEC DESCENDING_HI $TIME=2012/08:30:18:35:10
  @CEU_MACRO_EXEC DESCENDING_PL2 $TIME=2012/08:30:18:45:29

#  Orbit# 177 PERIGEE: Sun Precession Maneuver Commands  
  @FCT_SetScState housekeeping $TIME=2012/08:31:00:31:04
  @ECT_SetHTRCmd CATBED_5N_HTR,ON $TIME=2012/08:31:00:34:55
  @FCT_SetFcMode burn $TIME=2012/08:31:01:26:55
  @ACT_SetLrTarget ACS_SUN $TIME=2012/08:31:01:28:55
  @ACT_SetThrustTime 960 $TIME=2012/08:31:01:29:50
  @ACT_SetThrustEnable ENABLE $TIME=2012/08:31:01:29:55
  @ACT_SetThrustEnable DISABLE $TIME=2012/08:31:01:44:55
  @ECT_SetHTRCmd CATBED_5N_HTR,OFF $TIME=2012/08:31:01:44:55
  @ACT_SetThrustTime 0 $TIME=2012/08:31:01:45:25
  @FCT_SetFcMode Mission $TIME=2012/08:31:01:45:55

# Orbit# 177 PERIGEE: Battery Balancing 
  @ECT_SetLongEclipseFlag  TRUE  $TIME=2012/08:31:06:00:00
  @ECT_SetLongEclipseFlag  FALSE  $TIME=2012/08:31:07:30:00
end