[Isocops] IBEX Orbit# 232 ATS (4 Jan 14 - 13 Jan 14)
Ibex Mission Operations
ibexops at gmail.com
Sun Dec 22 18:52:29 EST 2013
Guys,
Here are the planning files and ATS for ORbit# 232.
Please respond to this email thread with any questions, comments and ATS
approvals.
*All approvals are required before 25 Dec 13 @ 1800 UTC*
Note the following:
1. IBEX_Hi ABAB Testing
Special Ops/Post-LUT Changes
Hi negative collimator voltage set to 1400
Hi ABAB (CEM comparison)
2. Moon in IBEX_Lo FOV
# 2014-01-05T18:45:46.525Z,MoonInLoFovStart,orbit:232
# 2014-01-06T09:02:44.473Z,MoonInLoFovStop,orbit:232
3. Battery Balancing at PERIGEE
SetLongEclipseFlag TRUE $TIME=2014/01:13:16:00:00
SetLongEclipseFlag FALSE $TIME=2014/01:13:17:30:00
4. Only APOGEE ground contact commands
5. PERIGEE ground contacts will be Blind_Acq contacts
--
Sheral R. Wesley
SPVR., Satellite Operations
IBEX Mission OPS
CYGNUS Mission Planning
(304) 279-6678
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; Filename: IBEX_2014_004_o0232a_v001.scr
; File type: MAESTRO Absolute Time Sequence Script (ATS)
;
; Create time: 2013/356.210229
; Plan period start: 2014/005.071600
; Plan period stop: 2014/014.035000
; Default time format: UTC
;
; Input files: 4
; IBEX_2014_004_o0232a_v001.oef
; IBEX_2014_004_o0232a_v003.stf
; IBEX_2013_forecast_26dec13_05feb14_v002.sap
; IBEX_2014_Orbit232_v001.caf
; ATS_CMD_TIME_OFFSET = 0
script ats_2014_01_05_07_16_00()
begin
# Orbit# 232 PERIGEE: Ascending BUS Commands
@ACT_SetSpinPulseProtectEnable Disable $TIME=2014/01:05:07:17:48
@FCT_SetScState science $TIME=2014/01:05:07:17:50
@ACT_SetSpinPulseProtectEnable Enable $TIME=2014/01:05:07:17:52
@CEU_LO_SCIENCE_MODE NORMAL $TIME=2014/01:05:07:17:54
# Orbit# 232 PERIGEE: Ascending Payload and Moon in Lo FOV Commands
# 2014-01-05T18:45:46.525Z,MoonInLoFovStart,orbit:232
# 2014-01-06T09:02:44.473Z,MoonInLoFovStop,orbit:232
@CEU_MACRO_EXEC ASCENDING_PL1 $TIME=2014/01:05:08:35:39
@CEU_MACRO_EXEC ASCENDING_HI $TIME=2014/01:05:08:35:55
@CEU_SET_PARAMETER 1, TLM_RATE_SOH $TIME=2014/01:05:08:46:57
@CEU_SET_PARAMETER 4, HV_STEP_DWELL $TIME=2014/01:05:08:47:00
@CEU_SET_PARAMETER 3, HV_STEP_FRAC $TIME=2014/01:05:08:47:04
@CEU_HI_COL_NEG_LVL 1400 $TIME=2014/01:05:08:47:08
@CEU_SET_PARAMETER 0, TLM_RATE_SOH $TIME=2014/01:05:08:47:43
@CEU_MACRO_EXEC ASCENDING_PL2 $TIME=2014/01:05:08:47:46
@CEU_MACRO_EXEC ASCENDING_PL1 $TIME=2014/01:05:08:49:51
@CEU_MACRO_EXEC ASCENDING_LO $TIME=2014/01:05:08:50:07
@CEU_MACRO_EXEC ASCENDING_PL2 $TIME=2014/01:05:08:58:27
@CEU_LO_PMT_LVL 300 $TIME=2014/01:05:20:29:09
@CEU_LO_IF_STAR_ADJ 0 $TIME=2014/01:05:20:29:11
@CEU_MODE HVENG $TIME=2014/01:06:05:33:46
@CEU_HI_CEM_1_LVL 1780 $TIME=2014/01:06:05:34:24
@CEU_HI_CEM_2_LVL 1780 $TIME=2014/01:06:05:34:54
@CEU_HI_CEM_3_LVL 1780 $TIME=2014/01:06:05:35:24
@CEU_MODE HVSCI $TIME=2014/01:06:05:35:54
@CEU_LO_IF_STAR_ADJ 250 $TIME=2014/01:06:07:49:14
@CEU_LO_PMT_LVL 800 $TIME=2014/01:06:07:49:16
@CEU_MODE HVENG $TIME=2014/01:07:02:06:58
@CEU_HI_CEM_1_LVL 1700 $TIME=2014/01:07:02:07:36
@CEU_HI_CEM_2_LVL 1700 $TIME=2014/01:07:02:08:06
@CEU_HI_CEM_3_LVL 1700 $TIME=2014/01:07:02:08:36
@CEU_MODE HVSCI $TIME=2014/01:07:02:09:06
@CEU_MODE HVENG $TIME=2014/01:07:22:40:10
@CEU_HI_CEM_1_LVL 1780 $TIME=2014/01:07:22:40:48
@CEU_HI_CEM_2_LVL 1780 $TIME=2014/01:07:22:41:18
@CEU_HI_CEM_3_LVL 1780 $TIME=2014/01:07:22:41:48
@CEU_MODE HVSCI $TIME=2014/01:07:22:42:18
# Orbit# 232 APOGEE: Descending Payload Commands
@CEU_MACRO_EXEC DESCENDING_PL1 $TIME=2014/01:08:19:13:25
@CEU_MACRO_EXEC DESCENDING_LO $TIME=2014/01:08:19:14:07
@CEU_MACRO_EXEC ASCENDING_PL2 $TIME=2014/01:08:19:22:29
@CEU_MACRO_EXEC DESCENDING_PL1 $TIME=2014/01:08:19:24:34
@CEU_MACRO_EXEC DESCENDING_HI $TIME=2014/01:08:19:25:16
@CEU_MACRO_EXEC DESCENDING_PL2 $TIME=2014/01:08:19:36:15
# Orbit# 232 APOGEE: Inertial Maneuver Commands
@FCT_SetScState housekeeping $TIME=2014/01:08:20:09:25
@ECT_SetHTRCmd CATBED_5N_HTR,ON $TIME=2014/01:08:20:14:23
@ACT_SetKFInputSelect GND_CMD, 0, 0, 0, 0 $TIME=2014/01:08:20:59:23
@ACT_SetEstUpdateEnables ENABLE, DISABLE $TIME=2014/01:08:20:59:24
@FCT_SetFcMode burn $TIME=2014/01:08:21:06:23
@ACT_SetInrDir 0.328832,-0.823598,-0.46212 $TIME=2014/01:08:21:07:23
@ACT_SetLrTarget ACS_INERTIAL $TIME=2014/01:08:21:08:23
@ACT_SetThrustTime 660 $TIME=2014/01:08:21:09:18
@ACT_SetThrustEnable ENABLE $TIME=2014/01:08:21:09:23
@ACT_SetThrustEnable DISABLE $TIME=2014/01:08:21:19:23
@ECT_SetHTRCmd CATBED_5N_HTR,OFF $TIME=2014/01:08:21:19:24
@ACT_SetThrustTime 0 $TIME=2014/01:08:21:19:53
@ACT_SetStaticZrate ESTIMATOR, 0.418 $TIME=2014/01:08:21:34:33
@ACT_SetKFInputSelect STA_PCT_VALID, 48,18,23,53 $TIME=2014/01:08:21:34:43
@FCT_SetFcMode Mission $TIME=2014/01:08:21:35:23
# Orbit# 232 APOGEE: Ascending BUS Commands
@ACT_SetSpinPulseProtectEnable Disable $TIME=2014/01:08:22:24:29
@FCT_SetScState science $TIME=2014/01:08:22:24:31
@ACT_SetSpinPulseProtectEnable Enable $TIME=2014/01:08:22:24:33
@CEU_LO_SCIENCE_MODE NORMAL $TIME=2014/01:08:22:24:35
# Orbit# 232 APOGEE: Ascending PAyload Commands
@CEU_MACRO_EXEC ASCENDING_PL1 $TIME=2014/01:08:22:54:29
@CEU_MACRO_EXEC ASCENDING_HI $TIME=2014/01:08:22:54:45
@CEU_SET_PARAMETER 1, TLM_RATE_SOH $TIME=2014/01:08:23:05:47
@CEU_SET_PARAMETER 4, HV_STEP_DWELL $TIME=2014/01:08:23:05:50
@CEU_SET_PARAMETER 3, HV_STEP_FRAC $TIME=2014/01:08:23:05:54
@CEU_HI_COL_NEG_LVL 1400 $TIME=2014/01:08:23:05:58
@CEU_SET_PARAMETER 0, TLM_RATE_SOH $TIME=2014/01:08:23:06:33
@CEU_MACRO_EXEC ASCENDING_PL2 $TIME=2014/01:08:23:06:36
@CEU_MACRO_EXEC ASCENDING_PL1 $TIME=2014/01:08:23:08:41
@CEU_MACRO_EXEC ASCENDING_LO $TIME=2014/01:08:23:08:57
@CEU_MACRO_EXEC ASCENDING_PL2 $TIME=2014/01:08:23:17:17
@CEU_MODE HVENG $TIME=2014/01:10:00:41:24
@CEU_HI_CEM_1_LVL 1780 $TIME=2014/01:10:00:42:02
@CEU_HI_CEM_2_LVL 1780 $TIME=2014/01:10:00:42:32
@CEU_HI_CEM_3_LVL 1780 $TIME=2014/01:10:00:43:02
@CEU_MODE HVSCI $TIME=2014/01:10:00:43:32
@CEU_MODE HVENG $TIME=2014/01:11:02:03:24
@CEU_HI_CEM_1_LVL 1700 $TIME=2014/01:11:02:04:02
@CEU_HI_CEM_2_LVL 1700 $TIME=2014/01:11:02:04:32
@CEU_HI_CEM_3_LVL 1700 $TIME=2014/01:11:02:05:02
@CEU_MODE HVSCI $TIME=2014/01:11:02:05:32
@CEU_MODE HVENG $TIME=2014/01:12:03:25:24
@CEU_HI_CEM_1_LVL 1780 $TIME=2014/01:12:03:26:02
@CEU_HI_CEM_2_LVL 1780 $TIME=2014/01:12:03:26:32
@CEU_HI_CEM_3_LVL 1780 $TIME=2014/01:12:03:27:02
@CEU_MODE HVSCI $TIME=2014/01:12:03:27:32
# Orbit# 232 APOGEE: Apogee Contact Commands
@ECT_SetRelay stx,on $TIME=2014/01:12:05:28:00
@FMI_SetDownlink2K $TIME=2014/01:12:05:28:02
@FMI_SetBilevelOutputControlReg STXMODE_Strobe,ON $TIME=2014/01:12:05:28:04
@FMI_SetBilevelOutputControlReg COHERENT,ON $TIME=2014/01:12:05:28:06
@ECT_SetRelay stx,off $TIME=2014/01:12:06:07:00
# Orbit# 232 PERIGEE: Descending Payload Commands
@CEU_MACRO_EXEC DESCENDING_PL1 $TIME=2014/01:13:04:47:26
@CEU_MACRO_EXEC DESCENDING_LO $TIME=2014/01:13:04:48:08
@CEU_MACRO_EXEC ASCENDING_PL2 $TIME=2014/01:13:04:56:30
@CEU_MACRO_EXEC DESCENDING_PL1 $TIME=2014/01:13:04:58:35
@CEU_MACRO_EXEC DESCENDING_HI $TIME=2014/01:13:04:59:17
@CEU_MACRO_EXEC DESCENDING_PL2 $TIME=2014/01:13:05:10:16
# Orbit# 232 PERIGEE: Inertial MAneuver Commands
@FCT_SetScState housekeeping $TIME=2014/01:13:05:59:42
@ECT_SetHTRCmd CATBED_5N_HTR,ON $TIME=2014/01:13:06:02:55
@ACT_SetKFInputSelect GND_CMD, 0, 0, 0, 0 $TIME=2014/01:13:06:47:55
@ACT_SetEstUpdateEnables ENABLE, DISABLE $TIME=2014/01:13:06:47:56
@FCT_SetFcMode burn $TIME=2014/01:13:06:54:55
@ACT_SetInrDir 0.411114,-0.793492,-0.448726 $TIME=2014/01:13:06:55:55
@ACT_SetLrTarget ACS_INERTIAL $TIME=2014/01:13:06:56:55
@ACT_SetThrustTime 660 $TIME=2014/01:13:06:57:50
@ACT_SetThrustEnable ENABLE $TIME=2014/01:13:06:57:55
@ACT_SetThrustEnable DISABLE $TIME=2014/01:13:07:07:55
@ECT_SetHTRCmd CATBED_5N_HTR,OFF $TIME=2014/01:13:07:07:56
@ACT_SetThrustTime 0 $TIME=2014/01:13:07:08:25
@ACT_SetStaticZrate ESTIMATOR, 0.418 $TIME=2014/01:13:07:23:05
@ACT_SetKFInputSelect STA_PCT_VALID, 48,18,23,53 $TIME=2014/01:13:07:23:15
@FCT_SetFcMode Mission $TIME=2014/01:13:07:23:55
# Orbit# 232 PERIGEE: Battery Balancing
@ECT_SetLongEclipseFlag TRUE $TIME=2014/01:13:16:00:00
@ECT_SetLongEclipseFlag FALSE $TIME=2014/01:13:17:30:00
end
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# Filename: IBEX_2014_004_o0232a_v001.ccvr
# File type: Command Load Constraint Violation Report (CCVR)
#
# Create time: 2013/356.210229
# Plan period start: 2014/005.071600
# Plan period stop: 2014/014.035000
# Default time format: UTC
#
# Input files: 1
# IBEX_2014_004_o0232a_v001.scr
==========================
HARD CONSTRAINT VIOLATIONS
==========================
NO VIOLATIONS.
==========================
SOFT CONSTRAINT VIOLATIONS
==========================
NO VIOLATIONS.
==============
OTHER MESSAGES
==============
NO MESSAGES.
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Orbit# 232
IBEX,USHI01,ADD,01/12/14,012,05:30:00,01/12/14,012,06:05:00,,LAHO 2K IBEX ORbit# 232 Apogee Contact (31 Desc)
IBEX,USHI01,ADD,01/13/14,013,07:00:00,01/13/14,013,08:00:00,,LAHO 320K IBEX ORbit# 232 SSR_Dump/Tracking Contact (14 Desc)
IBEX,AUWA01,ADD,01/13/14,013,22:30:00,01/13/14,013,23:30:00,,LAHO 160K IBEX ORbit# 232 SSR_Dump/Tracking Contact (10 Asc)
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