[Isocops] IBEX Orbit# 178 ATS (31 Aug 12 - 9 Sept 12)
Ibex Mission Operations
ibexops at gmail.com
Fri Aug 17 10:24:29 EDT 2012
Guys,
Here are the planning files and ATS for Orbit# 178.
All approvals/comments are required before 20 Aug 12 @1400 UTC
Please note the following:
*1. Orbit# 178 OEF*
- the OEF from Orbit# 176 was used to generate the file because of the sun
maneuver at PERIGEE of Orbit# 177
*2. IBEX_Lo and Moon in FOV commands have been deleted within the STF (Ken
Fairchild)
*- IBEX_Lo Recovery starts in Orbit# 177
- IBEX_Lo Star Sensor ATS for Orbit# 178 will be generated upon recovery
*3. Contact Commands*
- all contacts will remain as Blind_Acqs until we have recovered IBEX_Lo
to optimize stored command space within the FC
--
Sheral R. Wesley
SPVR., Satellite Operations
IBEX Mission OPS
(304) 279-6678
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; Filename: IBEX_2012_244_o0178a_v001.scr
; File type: MAESTRO Absolute Time Sequence Script (ATS)
;
; Create time: 2012/230.125511
; Plan period start: 2012/244.121400
; Plan period stop: 2012/253.153400
; Default time format: UTC
;
; Input files: 2
; IBEX_2012_244_o0178a_v001.oef
; IBEX_2012_244_o0178a_v002.stf
; ATS_CMD_TIME_OFFSET = 0
script ats_2012_08_31_12_14_00()
begin
# Orbit# 178 Ascending BUS Commands
@ACT_SetSpinPulseProtectEnable Disable $TIME=2012/08:31:12:16:23
@FCT_SetScState science $TIME=2012/08:31:12:16:25
@ACT_SetSpinPulseProtectEnable Enable $TIME=2012/08:31:12:16:27
@CEU_LO_SCIENCE_MODE NORMAL $TIME=2012/08:31:12:16:29
# Orbit# 178 Ascending IBEX_Hi Commands
@CEU_MACRO_EXEC ASCENDING_PL1 $TIME=2012/08:31:18:28:05
@CEU_MACRO_EXEC ASCENDING_HI $TIME=2012/08:31:18:28:21
@CEU_SET_PARAMETER 1, TLM_RATE_SOH $TIME=2012/08:31:18:39:15
@CEU_SET_PARAMETER 4, HV_STEP_DWELL $TIME=2012/08:31:18:39:18
@CEU_SET_PARAMETER 3, HV_STEP_FRAC $TIME=2012/08:31:18:39:22
@CEU_HI_CEM_4_LVL 1800 $TIME=2012/08:31:18:39:26
@CEU_SET_PARAMETER 0, TLM_RATE_SOH $TIME=2012/08:31:18:39:43
@CEU_MACRO_EXEC ASCENDING_PL2 $TIME=2012/08:31:18:39:46
# Orbit# 178 APOGEE: Descending IBEX_Hi Commands
@CEU_MACRO_EXEC DESCENDING_PL1 $TIME=2012/09:04:08:23:35
@CEU_MACRO_EXEC DESCENDING_HI $TIME=2012/09:04:08:24:17
@CEU_MACRO_EXEC DESCENDING_PL2 $TIME=2012/09:04:08:34:36
# Orbit# 178 APOGEE: Inertial Maneuver Commands
@FCT_SetScState housekeeping $TIME=2012/09:04:09:08:26
@ECT_SetHTRCmd CATBED_5N_HTR,ON $TIME=2012/09:04:09:16:05
@ACT_SetKFInputSelect GND_CMD, 0, 0, 0, 0 $TIME=2012/09:04:10:01:05
@ACT_SetEstUpdateEnables ENABLE, DISABLE $TIME=2012/09:04:10:01:06
@FCT_SetFcMode burn $TIME=2012/09:04:10:08:05
@ACT_SetInrDir -0.940397,0.316789,0.123688 $TIME=2012/09:04:10:09:05
@ACT_SetLrTarget ACS_INERTIAL $TIME=2012/09:04:10:10:05
@ACT_SetThrustTime 660 $TIME=2012/09:04:10:11:00
@ACT_SetThrustEnable ENABLE $TIME=2012/09:04:10:11:05
@ACT_SetThrustEnable DISABLE $TIME=2012/09:04:10:21:05
@ECT_SetHTRCmd CATBED_5N_HTR,OFF $TIME=2012/09:04:10:21:06
@ACT_SetThrustTime 0 $TIME=2012/09:04:10:21:35
@ACT_SetStaticZrate ESTIMATOR, 0.418 $TIME=2012/09:04:10:36:15
@ACT_SetKFInputSelect STA_PCT_VALID, 48,18,23,53 $TIME=2012/09:04:10:36:25
@FCT_SetFcMode Mission $TIME=2012/09:04:10:37:05
# Orbit# 178 APOGEE: Ascending BUS Commands
@ACT_SetSpinPulseProtectEnable Disable $TIME=2012/09:04:11:23:30
@FCT_SetScState science $TIME=2012/09:04:11:23:32
@ACT_SetSpinPulseProtectEnable Enable $TIME=2012/09:04:11:23:34
@CEU_LO_SCIENCE_MODE NORMAL $TIME=2012/09:04:11:23:36
# Orbit# 178 APOGEE: Ascending IBEX_Hi Commands
@CEU_MACRO_EXEC ASCENDING_PL1 $TIME=2012/09:04:11:53:30
@CEU_MACRO_EXEC ASCENDING_HI $TIME=2012/09:04:11:53:46
@CEU_SET_PARAMETER 1, TLM_RATE_SOH $TIME=2012/09:04:12:04:40
@CEU_SET_PARAMETER 4, HV_STEP_DWELL $TIME=2012/09:04:12:04:43
@CEU_SET_PARAMETER 3, HV_STEP_FRAC $TIME=2012/09:04:12:04:47
@CEU_HI_CEM_4_LVL 1800 $TIME=2012/09:04:12:04:51
@CEU_SET_PARAMETER 0, TLM_RATE_SOH $TIME=2012/09:04:12:05:08
@CEU_MACRO_EXEC ASCENDING_PL2 $TIME=2012/09:04:12:05:11
# Orbit# 178 PERIGEE: Descending IBEX_Hi Commands
@CEU_MACRO_EXEC DESCENDING_PL1 $TIME=2012/09:08:22:03:53
@CEU_MACRO_EXEC DESCENDING_HI $TIME=2012/09:08:22:04:35
@CEU_MACRO_EXEC DESCENDING_PL2 $TIME=2012/09:08:22:14:54
# Orbit# 178 PERIGEE: Inertial Maneuver Commands
@FCT_SetScState housekeeping $TIME=2012/09:09:04:11:09
@ECT_SetHTRCmd CATBED_5N_HTR,ON $TIME=2012/09:09:04:16:09
@ACT_SetKFInputSelect GND_CMD, 0, 0, 0, 0 $TIME=2012/09:09:05:01:09
@ACT_SetEstUpdateEnables ENABLE, DISABLE $TIME=2012/09:09:05:01:10
@FCT_SetFcMode burn $TIME=2012/09:09:05:08:09
@ACT_SetInrDir -0.964215,0.248035,0.093639 $TIME=2012/09:09:05:09:09
@ACT_SetLrTarget ACS_INERTIAL $TIME=2012/09:09:05:10:09
@ACT_SetThrustTime 660 $TIME=2012/09:09:05:11:04
@ACT_SetThrustEnable ENABLE $TIME=2012/09:09:05:11:09
@ACT_SetThrustEnable DISABLE $TIME=2012/09:09:05:21:09
@ECT_SetHTRCmd CATBED_5N_HTR,OFF $TIME=2012/09:09:05:21:10
@ACT_SetThrustTime 0 $TIME=2012/09:09:05:21:39
@ACT_SetStaticZrate ESTIMATOR, 0.418 $TIME=2012/09:09:05:36:19
@ACT_SetKFInputSelect STA_PCT_VALID, 48,18,23,53 $TIME=2012/09:09:05:36:29
@FCT_SetFcMode Mission $TIME=2012/09:09:05:37:09
end
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