[Isocops] IBEX Orbit# 182 ATS (6 Oct 12 - 16 Oct 12)
Ibex Mission Operations
ibexops at gmail.com
Tue Sep 25 09:44:51 EDT 2012
Guys,
Here are the planning files and ATS for Orbit# 182. The commands for
IBEX_Lo will be contained within another ATS
All approvals/comments are required before* 27 Sept 12 @0700 UTC*
**
**
*1. No contact commands within the ATS*
Orbit# 182
IBEX,USHI01,ADD,10/07/12,281,02:00:00,10/07/12,281,02:35:00,LAHO 40K IBEX
Orbit# 181 Tracking Contact (11 Asc)
IBEX,USHI01,ADD,10/12/12,286,02:30:00,10/12/12,286,03:05:00,,LAHO 2K IBEX
ORbit# 182 Apogee Contact (46 Desc)
IBEX,USHI01,ADD,10/15/12,289,15:00:00,10/15/12,289,16:00:00,,LAHO 320K IBEX
Orbit# 182 SSR_Dump/Tracking Contact (12 Desc)
*2. Battery Balancing during PERIGEE*
*3. **IBEX Command Violations:*
==========================
HARD CONSTRAINT VIOLATIONS
==========================
NO VIOLATIONS.
==========================
SOFT CONSTRAINT VIOLATIONS
==========================
NO VIOLATIONS.
--
Sheral R. Wesley
SPVR., Satellite Operations
IBEX Mission OPS
(304) 279-6678
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; Filename: IBEX_2012_280_o0182a_v001.scr
; File type: MAESTRO Absolute Time Sequence Script (ATS)
;
; Create time: 2012/269.113300
; Plan period start: 2012/281.010200
; Plan period stop: 2012/290.050500
; Default time format: UTC
;
; Input files: 2
; IBEX_2012_280_o0182a_v001.oef
; IBEX_2012_280_o0182a_v002.stf
; ATS_CMD_TIME_OFFSET = 0
script ats_2012_10_07_01_02_00()
begin
# Orbit# 182 Ascending BUS Commands
@ACT_SetSpinPulseProtectEnable Disable $TIME=2012/10:07:01:03:46
@FCT_SetScState science $TIME=2012/10:07:01:03:48
@ACT_SetSpinPulseProtectEnable Enable $TIME=2012/10:07:01:03:50
@CEU_LO_SCIENCE_MODE NORMAL $TIME=2012/10:07:01:03:52
# Orbit# 182 Ascending IBEX_Hi Commands
@CEU_MACRO_EXEC ASCENDING_PL1 $TIME=2012/10:07:07:39:49
@CEU_MACRO_EXEC ASCENDING_HI $TIME=2012/10:07:07:40:05
@CEU_SET_PARAMETER 1, TLM_RATE_SOH $TIME=2012/10:07:07:50:59
@CEU_SET_PARAMETER 4, HV_STEP_DWELL $TIME=2012/10:07:07:51:02
@CEU_SET_PARAMETER 3, HV_STEP_FRAC $TIME=2012/10:07:07:51:06
@CEU_HI_CEM_4_LVL 1800 $TIME=2012/10:07:07:51:10
@CEU_SET_PARAMETER 0, TLM_RATE_SOH $TIME=2012/10:07:07:51:27
@CEU_MACRO_EXEC ASCENDING_PL2 $TIME=2012/10:07:07:51:30
# Orbit# 182 APOGEE: Descending IBEX_Hi Commands
@CEU_MACRO_EXEC DESCENDING_PL1 $TIME=2012/10:10:21:51:34
@CEU_MACRO_EXEC DESCENDING_HI $TIME=2012/10:10:21:52:16
@CEU_MACRO_EXEC DESCENDING_PL2 $TIME=2012/10:10:22:02:35
# Orbit# 182 APOGEE: Inertial Maneuver Commands
@FCT_SetScState housekeeping $TIME=2012/10:10:22:36:25
@ECT_SetHTRCmd CATBED_5N_HTR,ON $TIME=2012/10:10:22:41:23
@ACT_SetKFInputSelect GND_CMD, 0, 0, 0, 0 $TIME=2012/10:10:23:26:23
@ACT_SetEstUpdateEnables ENABLE, DISABLE $TIME=2012/10:10:23:26:24
@FCT_SetFcMode burn $TIME=2012/10:10:23:33:23
@ACT_SetInrDir -0.96195,-0.24543,-0.120068 $TIME=2012/10:10:23:34:23
@ACT_SetLrTarget ACS_INERTIAL $TIME=2012/10:10:23:35:23
@ACT_SetThrustTime 660 $TIME=2012/10:10:23:36:18
@ACT_SetThrustEnable ENABLE $TIME=2012/10:10:23:36:23
@ACT_SetThrustEnable DISABLE $TIME=2012/10:10:23:46:23
@ECT_SetHTRCmd CATBED_5N_HTR,OFF $TIME=2012/10:10:23:46:24
@ACT_SetThrustTime 0 $TIME=2012/10:10:23:46:53
@ACT_SetStaticZrate ESTIMATOR, 0.418 $TIME=2012/10:11:00:01:33
@ACT_SetKFInputSelect STA_PCT_VALID, 48,18,23,53 $TIME=2012/10:11:00:01:43
@FCT_SetFcMode Mission $TIME=2012/10:11:00:02:23
# Orbit# 182 APOGEE: Ascending BUS Commands
@ACT_SetSpinPulseProtectEnable Disable $TIME=2012/10:11:00:51:29
@FCT_SetScState science $TIME=2012/10:11:00:51:31
@ACT_SetSpinPulseProtectEnable Enable $TIME=2012/10:11:00:51:33
@CEU_LO_SCIENCE_MODE NORMAL $TIME=2012/10:11:00:51:35
# Orbit# 182 APOGEE: Ascending IBEX_Hi Commands
@CEU_MACRO_EXEC ASCENDING_PL1 $TIME=2012/10:11:01:21:29
@CEU_MACRO_EXEC ASCENDING_HI $TIME=2012/10:11:01:21:45
@CEU_SET_PARAMETER 1, TLM_RATE_SOH $TIME=2012/10:11:01:32:39
@CEU_SET_PARAMETER 4, HV_STEP_DWELL $TIME=2012/10:11:01:32:42
@CEU_SET_PARAMETER 3, HV_STEP_FRAC $TIME=2012/10:11:01:32:46
@CEU_HI_CEM_4_LVL 1800 $TIME=2012/10:11:01:32:50
@CEU_SET_PARAMETER 0, TLM_RATE_SOH $TIME=2012/10:11:01:33:07
@CEU_MACRO_EXEC ASCENDING_PL2 $TIME=2012/10:11:01:33:10
# Orbit# 182 PERIGEE: Descending IBEX_Hi Commands
@CEU_MACRO_EXEC DESCENDING_PL1 $TIME=2012/10:15:11:49:42
@CEU_MACRO_EXEC DESCENDING_HI $TIME=2012/10:15:11:50:24
@CEU_MACRO_EXEC DESCENDING_PL2 $TIME=2012/10:15:12:00:43
# Orbit# 182 PERIGEE: Inertial Maneuver Commands
@FCT_SetScState housekeeping $TIME=2012/10:15:18:20:09
@ECT_SetHTRCmd CATBED_5N_HTR,ON $TIME=2012/10:15:18:24:36
@ACT_SetKFInputSelect GND_CMD, 0, 0, 0, 0 $TIME=2012/10:15:19:09:36
@ACT_SetEstUpdateEnables ENABLE, DISABLE $TIME=2012/10:15:19:09:37
@FCT_SetFcMode burn $TIME=2012/10:15:19:16:36
@ACT_SetInrDir -0.936985,-0.315276,-0.150536 $TIME=2012/10:15:19:17:36
@ACT_SetLrTarget ACS_INERTIAL $TIME=2012/10:15:19:18:36
@ACT_SetThrustTime 660 $TIME=2012/10:15:19:19:31
@ACT_SetThrustEnable ENABLE $TIME=2012/10:15:19:19:36
@ACT_SetThrustEnable DISABLE $TIME=2012/10:15:19:29:36
@ECT_SetHTRCmd CATBED_5N_HTR,OFF $TIME=2012/10:15:19:29:37
@ACT_SetThrustTime 0 $TIME=2012/10:15:19:30:06
@ACT_SetStaticZrate ESTIMATOR, 0.418 $TIME=2012/10:15:19:44:46
@ACT_SetKFInputSelect STA_PCT_VALID, 48,18,23,53 $TIME=2012/10:15:19:44:56
@FCT_SetFcMode Mission $TIME=2012/10:15:19:45:36
# Orbit# 182 PERIGEE: Battery Balancing
@ECT_SetLongEclipseFlag TRUE $TIME=2012/10:16:01:00:00
@ECT_SetLongEclipseFlag FALSE $TIME=2012/10:16:02:30:00
end
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Orbit# 182
IBEX,USHI01,ADD,10/07/12,281,02:00:00,10/07/12,281,02:35:00,LAHO 40K IBEX Orbit# 181 Tracking Contact (11 Asc)
IBEX,USHI01,ADD,10/12/12,286,02:30:00,10/12/12,286,03:05:00,,LAHO 2K IBEX ORbit# 182 Apogee Contact (46 Desc)
IBEX,USHI01,ADD,10/15/12,289,15:00:00,10/15/12,289,16:00:00,,LAHO 320K IBEX Orbit# 182 SSR_Dump/Tracking Contact (12 Desc)
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