[Isocops] IBEX Orbit# 185 ATS (2 Nov 12 - 11 Nov 12)
Ibex Mission Operations
ibexops at gmail.com
Mon Oct 22 13:48:42 EDT 2012
Guys,
Here are the planning files for the various Orbit# 185 ATS command loads.
Approvals are required before 25 Oct 12 @ 1800 UTC
*1. IBEX_2012_307_o0185a_v001.scr*
- Nominal ATS commands with the new LUT settings
- Contains BUS, IBEX_Hi and IBEX_Lo Payload Commands
- Contains battery cell balancing commands at Perigee
- Does NOT contain contact commands
- CCVR has no command violations
*2. IBEX_2012_307_o0185a_NoLo_v001.scr*
- Contains IBEX-Hi Payload and BUS Commands
- Contains NO IBEX_Lo Payload Commands
- Contains Inertial MAneuver Commands
- Contains battery cell balancing commands at Perigee
- Does NOT contain contact commands
- CCVR has no command violations
*3. IBEX_2012_307_o0185a_Lo_Commands_v001.scr*
- Contains IBEX_Lo Commands Only
- Contains Moon in Lo FOV Commands
- Inertial Maneuver commands are commented out
- CCVR violations are from using ONLY IBEX_Lo commands to generate the ATS
SOFT CONSTRAINT VIOLATIONS
==========================
IBX-CLC-003: Payload mode is HVSCI during interval 2012/11/06 21:51:10 UTC -
2012/11/06 22:01:10 UTC, which overlaps 5N thruster maneuver at
2012/11/06 21:51:10 UTC - 2012/11/06 22:01:10 UTC
IBX-CLC-003: Payload mode is HVSCI during interval 2012/11/11 15:57:47 UTC -
2012/11/11 16:07:47 UTC, which overlaps 5N thruster maneuver at
2012/11/11 15:57:47 UTC - 2012/11/11 16:07:47 UTC
IBX-CLC-008: Spacecraft state is HK during interval 2012/11/03 07:36:47 UTC
-
2012/11/06 23:50:02 UTC, which overlaps HVSCI payload mode at
2012/11/03 07:36:47 UTC - 2012/11/06 23:50:02 UTC
IBX-CLC-008: Spacecraft state is HK during interval 2012/11/06 23:50:02 UTC
-
2012/11/12 01:23:00 UTC, which overlaps HVSCI payload mode at
2012/11/06 23:50:02 UTC - 2012/11/12 01:23:00 UTC
IBX-CLC-009: Payload mode is HVSCI during interval 2012/11/11 15:28:21 UTC -
2012/11/12 01:23:00 UTC, which overlaps times when IBEX is
under 10
RE at 2012/11/11 15:28:21 UTC - 2012/11/12 01:23:00 UTC
--
Sheral R. Wesley
SPVR., Satellite Operations
IBEX Mission OPS
(304) 279-6678
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; Filename: IBEX_2012_307_o0185a_v001.scr
; File type: MAESTRO Absolute Time Sequence Script (ATS)
;
; Create time: 2012/296.164222
; Plan period start: 2012/308.002500
; Plan period stop: 2012/317.012300
; Default time format: UTC
;
; Input files: 2
; IBEX_2012_307_o0185a_v001.oef
; IBEX_2012_307_o0185a_v001.stf
; ATS_CMD_TIME_OFFSET = 0
script ats_2012_11_03_00_25_00()
begin
# Orbit# 185 Ascending BUS Commands
@ACT_SetSpinPulseProtectEnable Disable $TIME=2012/11:03:00:26:05
@FCT_SetScState science $TIME=2012/11:03:00:26:07
@ACT_SetSpinPulseProtectEnable Enable $TIME=2012/11:03:00:26:09
@CEU_LO_SCIENCE_MODE NORMAL $TIME=2012/11:03:00:26:11
# Orbit# 185 Ascending Payload Commands
@CEU_MACRO_EXEC ASCENDING_PL1 $TIME=2012/11:03:07:23:01
@CEU_MACRO_EXEC ASCENDING_HI $TIME=2012/11:03:07:23:17
@CEU_MACRO_EXEC ASCENDING_PL2 $TIME=2012/11:03:07:34:19
@CEU_MACRO_EXEC ASCENDING_PL1 $TIME=2012/11:03:07:36:24
@CEU_MACRO_EXEC ASCENDING_LO $TIME=2012/11:03:07:36:40
@CEU_MACRO_EXEC ASCENDING_PL2 $TIME=2012/11:03:07:45:00
# Orbit# 185 Moon in Lo FOV
# 2012-11-06T21:58:11.498Z,MoonInLoFovStart,orbit:185
# 2012-11-07T02:55:01.297Z,MoonInLoFovStop,orbit:185
@CEU_LO_PMT_LVL 300 $TIME=2012/11:05:21:05:41
@CEU_LO_IF_STAR_ADJ 0 $TIME=2012/11:05:21:05:43
# Orbit# 185 APOGEE: Descending Payload Commands
@CEU_MACRO_EXEC DESCENDING_PL1 $TIME=2012/11:06:19:55:12
@CEU_MACRO_EXEC DESCENDING_LO $TIME=2012/11:06:19:55:54
@CEU_MACRO_EXEC ASCENDING_PL2 $TIME=2012/11:06:20:04:16
@CEU_MACRO_EXEC DESCENDING_PL1 $TIME=2012/11:06:20:06:21
@CEU_MACRO_EXEC DESCENDING_HI $TIME=2012/11:06:20:07:03
@CEU_MACRO_EXEC DESCENDING_PL2 $TIME=2012/11:06:20:18:02
# Orbit# 185 APOGEE: Inertial MAneuver Commands
@FCT_SetScState housekeeping $TIME=2012/11:06:20:51:12
@ECT_SetHTRCmd CATBED_5N_HTR,ON $TIME=2012/11:06:20:56:10
@ACT_SetKFInputSelect GND_CMD, 0, 0, 0, 0 $TIME=2012/11:06:21:41:10
@ACT_SetEstUpdateEnables ENABLE, DISABLE $TIME=2012/11:06:21:41:11
@FCT_SetFcMode burn $TIME=2012/11:06:21:48:10
@ACT_SetInrDir -0.735578,-0.616458,-0.280901 $TIME=2012/11:06:21:49:10
@ACT_SetLrTarget ACS_INERTIAL $TIME=2012/11:06:21:50:10
@ACT_SetThrustTime 660 $TIME=2012/11:06:21:51:05
@ACT_SetThrustEnable ENABLE $TIME=2012/11:06:21:51:10
@ACT_SetThrustEnable DISABLE $TIME=2012/11:06:22:01:10
@ECT_SetHTRCmd CATBED_5N_HTR,OFF $TIME=2012/11:06:22:01:11
@ACT_SetThrustTime 0 $TIME=2012/11:06:22:01:40
@ACT_SetStaticZrate ESTIMATOR, 0.418 $TIME=2012/11:06:22:16:20
@ACT_SetKFInputSelect STA_PCT_VALID, 48,18,23,53 $TIME=2012/11:06:22:16:30
@FCT_SetFcMode Mission $TIME=2012/11:06:22:17:10
# Orbit# 185 APOGEE: Ascending BUS Commands
@ACT_SetSpinPulseProtectEnable Disable $TIME=2012/11:06:23:06:16
@FCT_SetScState science $TIME=2012/11:06:23:06:18
@ACT_SetSpinPulseProtectEnable Enable $TIME=2012/11:06:23:06:20
@CEU_LO_SCIENCE_MODE NORMAL $TIME=2012/11:06:23:06:22
# Orbit# 185 APOGEE: Ascending Payload Commands
@CEU_MACRO_EXEC ASCENDING_PL1 $TIME=2012/11:06:23:36:16
@CEU_MACRO_EXEC ASCENDING_HI $TIME=2012/11:06:23:36:32
@CEU_MACRO_EXEC ASCENDING_PL2 $TIME=2012/11:06:23:47:34
@CEU_MACRO_EXEC ASCENDING_PL1 $TIME=2012/11:06:23:49:39
@CEU_MACRO_EXEC ASCENDING_LO $TIME=2012/11:06:23:49:55
@CEU_MACRO_EXEC ASCENDING_PL2 $TIME=2012/11:06:23:58:15
# Orbit# 185 PERIGEE: Descending Payload Commands
@CEU_MACRO_EXEC DESCENDING_PL1 $TIME=2012/11:11:08:03:52
@CEU_MACRO_EXEC DESCENDING_LO $TIME=2012/11:11:08:04:34
@CEU_MACRO_EXEC ASCENDING_PL2 $TIME=2012/11:11:08:12:56
@CEU_MACRO_EXEC DESCENDING_PL1 $TIME=2012/11:11:08:15:01
@CEU_MACRO_EXEC DESCENDING_HI $TIME=2012/11:11:08:15:43
@CEU_MACRO_EXEC DESCENDING_PL2 $TIME=2012/11:11:08:26:42
# Orbit# 185 PERIGEE: Inertial Maneuver Commands
@FCT_SetScState housekeeping $TIME=2012/11:11:14:58:21
@ECT_SetHTRCmd CATBED_5N_HTR,ON $TIME=2012/11:11:15:02:47
@ACT_SetKFInputSelect GND_CMD, 0, 0, 0, 0 $TIME=2012/11:11:15:47:47
@ACT_SetEstUpdateEnables ENABLE, DISABLE $TIME=2012/11:11:15:47:48
@FCT_SetFcMode burn $TIME=2012/11:11:15:54:47
@ACT_SetInrDir -0.679541,-0.667946,-0.303434 $TIME=2012/11:11:15:55:47
@ACT_SetLrTarget ACS_INERTIAL $TIME=2012/11:11:15:56:47
@ACT_SetThrustTime 660 $TIME=2012/11:11:15:57:42
@ACT_SetThrustEnable ENABLE $TIME=2012/11:11:15:57:47
@ACT_SetThrustEnable DISABLE $TIME=2012/11:11:16:07:47
@ECT_SetHTRCmd CATBED_5N_HTR,OFF $TIME=2012/11:11:16:07:48
@ACT_SetThrustTime 0 $TIME=2012/11:11:16:08:17
@ACT_SetStaticZrate ESTIMATOR, 0.418 $TIME=2012/11:11:16:22:57
@ACT_SetKFInputSelect STA_PCT_VALID, 48,18,23,53 $TIME=2012/11:11:16:23:07
@FCT_SetFcMode Mission $TIME=2012/11:11:16:23:47
# Orbit# 185 PERIGEE: Battery Balancing
@ECT_SetLongEclipseFlag TRUE $TIME=2012/11:11:20:00:00
@ECT_SetLongEclipseFlag FALSE $TIME=2012/11:11:21:30:00
end
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; Filename: IBEX_2012_307_o0185a_NoLo_v001.scr
; File type: MAESTRO Absolute Time Sequence Script (ATS)
;
; Create time: 2012/296.160732
; Plan period start: 2012/308.002500
; Plan period stop: 2012/317.012300
; Default time format: UTC
;
; Input files: 2
; IBEX_2012_307_o0185a_v001.oef
; IBEX_2012_307_o0185a_NoLo_v001.stf
; ATS_CMD_TIME_OFFSET = 0
script ats_2012_11_03_00_25_00()
begin
# ORbit# 185 Ascending BUS Commands
@ACT_SetSpinPulseProtectEnable Disable $TIME=2012/11:03:00:26:05
@FCT_SetScState science $TIME=2012/11:03:00:26:07
@ACT_SetSpinPulseProtectEnable Enable $TIME=2012/11:03:00:26:09
@CEU_LO_SCIENCE_MODE NORMAL $TIME=2012/11:03:00:26:11
# Orbit# 185 Ascending IBEX_Hi Commands
@CEU_MACRO_EXEC ASCENDING_PL1 $TIME=2012/11:03:07:23:01
@CEU_MACRO_EXEC ASCENDING_HI $TIME=2012/11:03:07:23:17
@CEU_SET_PARAMETER 1, TLM_RATE_SOH $TIME=2012/11:03:07:34:11
@CEU_SET_PARAMETER 4, HV_STEP_DWELL $TIME=2012/11:03:07:34:14
@CEU_SET_PARAMETER 3, HV_STEP_FRAC $TIME=2012/11:03:07:34:18
@CEU_HI_CEM_4_LVL 1800 $TIME=2012/11:03:07:34:22
@CEU_SET_PARAMETER 0, TLM_RATE_SOH $TIME=2012/11:03:07:34:39
@CEU_MACRO_EXEC ASCENDING_PL2 $TIME=2012/11:03:07:34:42
# Orbit# 185 APOGEE: Descending IBEX_Hi Commands
@CEU_MACRO_EXEC DESCENDING_PL1 $TIME=2012/11:06:20:06:21
@CEU_MACRO_EXEC DESCENDING_HI $TIME=2012/11:06:20:07:03
@CEU_MACRO_EXEC DESCENDING_PL2 $TIME=2012/11:06:20:17:22
# Orbit# 185 APOGEE: Inertial MAneuver Commands
@FCT_SetScState housekeeping $TIME=2012/11:06:20:51:12
@ECT_SetHTRCmd CATBED_5N_HTR,ON $TIME=2012/11:06:20:56:10
@ACT_SetKFInputSelect GND_CMD, 0, 0, 0, 0 $TIME=2012/11:06:21:41:10
@ACT_SetEstUpdateEnables ENABLE, DISABLE $TIME=2012/11:06:21:41:11
@FCT_SetFcMode burn $TIME=2012/11:06:21:48:10
@ACT_SetInrDir -0.735578,-0.616458,-0.280901 $TIME=2012/11:06:21:49:10
@ACT_SetLrTarget ACS_INERTIAL $TIME=2012/11:06:21:50:10
@ACT_SetThrustTime 660 $TIME=2012/11:06:21:51:05
@ACT_SetThrustEnable ENABLE $TIME=2012/11:06:21:51:10
@ACT_SetThrustEnable DISABLE $TIME=2012/11:06:22:01:10
@ECT_SetHTRCmd CATBED_5N_HTR,OFF $TIME=2012/11:06:22:01:11
@ACT_SetThrustTime 0 $TIME=2012/11:06:22:01:40
@ACT_SetStaticZrate ESTIMATOR, 0.418 $TIME=2012/11:06:22:16:20
@ACT_SetKFInputSelect STA_PCT_VALID, 48,18,23,53 $TIME=2012/11:06:22:16:30
@FCT_SetFcMode Mission $TIME=2012/11:06:22:17:10
# Orbit# 185 APOGEE: Ascending BUS Commands
@ACT_SetSpinPulseProtectEnable Disable $TIME=2012/11:06:23:06:16
@FCT_SetScState science $TIME=2012/11:06:23:06:18
@ACT_SetSpinPulseProtectEnable Enable $TIME=2012/11:06:23:06:20
@CEU_LO_SCIENCE_MODE NORMAL $TIME=2012/11:06:23:06:22
# Orbit# 185 APOGEE: Ascending IBEX_Hi Commands
@CEU_MACRO_EXEC ASCENDING_PL1 $TIME=2012/11:06:23:36:16
@CEU_MACRO_EXEC ASCENDING_HI $TIME=2012/11:06:23:36:32
@CEU_SET_PARAMETER 1, TLM_RATE_SOH $TIME=2012/11:06:23:47:26
@CEU_SET_PARAMETER 4, HV_STEP_DWELL $TIME=2012/11:06:23:47:29
@CEU_SET_PARAMETER 3, HV_STEP_FRAC $TIME=2012/11:06:23:47:33
@CEU_HI_CEM_4_LVL 1800 $TIME=2012/11:06:23:47:37
@CEU_SET_PARAMETER 0, TLM_RATE_SOH $TIME=2012/11:06:23:47:54
@CEU_MACRO_EXEC ASCENDING_PL2 $TIME=2012/11:06:23:47:57
# Orbit# 185 PERIGEE: Descending IBEX_Hi Commands
@CEU_MACRO_EXEC DESCENDING_PL1 $TIME=2012/11:11:08:15:01
@CEU_MACRO_EXEC DESCENDING_HI $TIME=2012/11:11:08:15:43
@CEU_MACRO_EXEC DESCENDING_PL2 $TIME=2012/11:11:08:26:02
# Orbit# 185 PERIGEE: Inertial Maneuver Commands
@FCT_SetScState housekeeping $TIME=2012/11:11:14:58:21
@ECT_SetHTRCmd CATBED_5N_HTR,ON $TIME=2012/11:11:15:02:47
@ACT_SetKFInputSelect GND_CMD, 0, 0, 0, 0 $TIME=2012/11:11:15:47:47
@ACT_SetEstUpdateEnables ENABLE, DISABLE $TIME=2012/11:11:15:47:48
@FCT_SetFcMode burn $TIME=2012/11:11:15:54:47
@ACT_SetInrDir -0.679541,-0.667946,-0.303434 $TIME=2012/11:11:15:55:47
@ACT_SetLrTarget ACS_INERTIAL $TIME=2012/11:11:15:56:47
@ACT_SetThrustTime 660 $TIME=2012/11:11:15:57:42
@ACT_SetThrustEnable ENABLE $TIME=2012/11:11:15:57:47
@ACT_SetThrustEnable DISABLE $TIME=2012/11:11:16:07:47
@ECT_SetHTRCmd CATBED_5N_HTR,OFF $TIME=2012/11:11:16:07:48
@ACT_SetThrustTime 0 $TIME=2012/11:11:16:08:17
@ACT_SetStaticZrate ESTIMATOR, 0.418 $TIME=2012/11:11:16:22:57
@ACT_SetKFInputSelect STA_PCT_VALID, 48,18,23,53 $TIME=2012/11:11:16:23:07
@FCT_SetFcMode Mission $TIME=2012/11:11:16:23:47
# Orbit# 185 PERIGEE: Battery Balancing
@ECT_SetLongEclipseFlag TRUE $TIME=2012/11:11:20:00:00
@ECT_SetLongEclipseFlag FALSE $TIME=2012/11:11:21:30:00
end
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; Filename: IBEX_2012_307_o0185a_Lo_Commands_v001.scr
; File type: MAESTRO Absolute Time Sequence Script (ATS)
;
; Create time: 2012/296.154841
; Plan period start: 2012/308.002500
; Plan period stop: 2012/317.012300
; Default time format: UTC
;
; Input files: 2
; IBEX_2012_307_o0185a_v001.oef
; IBEX_2012_307_o0185a_Lo_Commands_v001.stf
; ATS_CMD_TIME_OFFSET = 0
script ats_2012_11_03_00_25_00()
begin
# Orbit# 185 Ascending IBEX_Lo Commands with Moon in Lo FOV Commands
# 2012-11-06T21:58:11.498Z,MoonInLoFovStart,orbit:185
# 2012-11-07T02:55:01.297Z,MoonInLoFovStop,orbit:185
@CEU_MACRO_EXEC ASCENDING_PL1 $TIME=2012/11:03:07:36:47
@CEU_SET_PARAMETER 1, TLM_RATE_SOH_LO $TIME=2012/11:03:07:37:03
@CEU_SET_PARAMETER 4, HV_STEP_DWELL $TIME=2012/11:03:07:37:12
@CEU_SET_PARAMETER 16, HV_STEP_FRAC $TIME=2012/11:03:07:37:14
@CEU_LO_PMT_LVL 800 $TIME=2012/11:03:07:37:15
@CEU_SET_PARAMETER 1, HV_STEP_FRAC $TIME=2012/11:03:07:37:38
@CEU_SET_PARAMETER 11, HV_STEP_FRAC $TIME=2012/11:03:07:37:54
@CEU_LO_COL_NEG_LVL 400 $TIME=2012/11:03:07:37:56
@CEU_SET_PARAMETER 1, HV_STEP_FRAC $TIME=2012/11:03:07:39:17
@CEU_LO_IF_PAC_VSET 7000 $TIME=2012/11:03:07:39:19
@CEU_LO_IF_MCP_VSET 2854 $TIME=2012/11:03:07:42:11
@CEU_SET_PARAMETER 0, HV_STEP_DWELL $TIME=2012/11:03:07:44:31
@CEU_SET_PARAMETER 255, HV_STEP_FRAC $TIME=2012/11:03:07:44:33
@CEU_LO_U_POS_LVL 0 $TIME=2012/11:03:07:44:35
@CEU_LO_U_NEG_LVL 0 $TIME=2012/11:03:07:44:49
@CEU_SET_PARAMETER 4, HV_STEP_DWELL $TIME=2012/11:03:07:45:05
@CEU_SET_PARAMETER 1, HV_STEP_FRAC $TIME=2012/11:03:07:45:07
@CEU_SET_PARAMETER 0, TLM_RATE_SOH_LO $TIME=2012/11:03:07:45:08
@CEU_MACRO_EXEC ASCENDING_PL2 $TIME=2012/11:03:07:45:25
@CEU_LO_PMT_LVL 300 $TIME=2012/11:05:21:05:41
@CEU_LO_IF_STAR_ADJ 0 $TIME=2012/11:05:21:05:43
# Orbit# 185 APOGEE: Descending IBEX_Lo Commands
@CEU_MACRO_EXEC DESCENDING_PL1 $TIME=2012/11:06:19:55:12
@CEU_SET_PARAMETER 4, HV_STEP_DWELL $TIME=2012/11:06:19:55:56
@CEU_SET_PARAMETER 16, HV_STEP_FRAC $TIME=2012/11:06:19:55:58
@CEU_LO_PMT_LVL 640 $TIME=2012/11:06:19:56:01
@CEU_SET_PARAMETER 1, HV_STEP_FRAC $TIME=2012/11:06:19:56:24
@CEU_LO_IF_PAC_VSET 5500 $TIME=2012/11:06:19:56:26
@CEU_LO_IF_MCP_VSET 2083 $TIME=2012/11:06:19:59:18
@CEU_SET_PARAMETER 11, HV_STEP_FRAC $TIME=2012/11:06:20:02:02
@CEU_LO_COL_NEG_LVL 216 $TIME=2012/11:06:20:02:04
@CEU_SET_PARAMETER 0, HV_STEP_DWELL $TIME=2012/11:06:20:03:20
@CEU_SET_PARAMETER 255, HV_STEP_FRAC $TIME=2012/11:06:20:03:22
@CEU_LO_U_POS_LVL 0 $TIME=2012/11:06:20:03:23
@CEU_LO_U_NEG_LVL 0 $TIME=2012/11:06:20:03:37
@CEU_SET_PARAMETER 4, HV_STEP_DWELL $TIME=2012/11:06:20:03:52
@CEU_SET_PARAMETER 1, HV_STEP_FRAC $TIME=2012/11:06:20:03:54
@CEU_MACRO_EXEC ASCENDING_PL2 $TIME=2012/11:06:20:04:16
# Orbit# 185 APOGEE: Inertial MAneuver Commands
# @ECT_SetHTRCmd CATBED_5N_HTR,ON $TIME=2012/11:06:20:56:10
# @ACT_SetKFInputSelect GND_CMD, 0, 0, 0, 0 $TIME=2012/11:06:21:41:10
# @ACT_SetEstUpdateEnables ENABLE, DISABLE $TIME=2012/11:06:21:41:11
# @FCT_SetFcMode burn $TIME=2012/11:06:21:48:10
# @ACT_SetInrDir -0.735578,-0.616458,-0.280901 $TIME=2012/11:06:21:49:10
# @ACT_SetLrTarget ACS_INERTIAL $TIME=2012/11:06:21:50:10
# @ACT_SetThrustTime 660 $TIME=2012/11:06:21:51:05
# @ACT_SetThrustEnable ENABLE $TIME=2012/11:06:21:51:10
# @ACT_SetThrustEnable DISABLE $TIME=2012/11:06:22:01:10
# @ECT_SetHTRCmd CATBED_5N_HTR,OFF $TIME=2012/11:06:22:01:11
# @ACT_SetThrustTime 0 $TIME=2012/11:06:22:01:40
# @ACT_SetStaticZrate ESTIMATOR, 0.418 $TIME=2012/11:06:22:16:20
# @ACT_SetKFInputSelect STA_PCT_VALID, 48,18,23,53 $TIME=2012/11:06:22:16:30
# @FCT_SetFcMode Mission $TIME=2012/11:06:22:17:10
# Orbit# 185 APOGEE: Ascending IBEX_Lo Commands
@CEU_MACRO_EXEC ASCENDING_PL1 $TIME=2012/11:06:23:50:02
@CEU_SET_PARAMETER 1, TLM_RATE_SOH_LO $TIME=2012/11:06:23:50:18
@CEU_SET_PARAMETER 4, HV_STEP_DWELL $TIME=2012/11:06:23:50:27
@CEU_SET_PARAMETER 16, HV_STEP_FRAC $TIME=2012/11:06:23:50:29
@CEU_LO_PMT_LVL 800 $TIME=2012/11:06:23:50:30
@CEU_SET_PARAMETER 1, HV_STEP_FRAC $TIME=2012/11:06:23:50:53
@CEU_SET_PARAMETER 11, HV_STEP_FRAC $TIME=2012/11:06:23:51:09
@CEU_LO_COL_NEG_LVL 400 $TIME=2012/11:06:23:51:11
@CEU_SET_PARAMETER 1, HV_STEP_FRAC $TIME=2012/11:06:23:52:32
@CEU_LO_IF_PAC_VSET 7000 $TIME=2012/11:06:23:52:34
@CEU_LO_IF_MCP_VSET 2854 $TIME=2012/11:06:23:55:26
@CEU_SET_PARAMETER 0, HV_STEP_DWELL $TIME=2012/11:06:23:57:46
@CEU_SET_PARAMETER 255, HV_STEP_FRAC $TIME=2012/11:06:23:57:48
@CEU_LO_U_POS_LVL 0 $TIME=2012/11:06:23:57:50
@CEU_LO_U_NEG_LVL 0 $TIME=2012/11:06:23:58:04
@CEU_SET_PARAMETER 4, HV_STEP_DWELL $TIME=2012/11:06:23:58:20
@CEU_SET_PARAMETER 1, HV_STEP_FRAC $TIME=2012/11:06:23:58:22
@CEU_SET_PARAMETER 0, TLM_RATE_SOH_LO $TIME=2012/11:06:23:58:23
@CEU_MACRO_EXEC ASCENDING_PL2 $TIME=2012/11:06:23:58:40
# Orbit# 185 PERIGEE: Descending IBEX_Lo Commands
@CEU_MACRO_EXEC DESCENDING_PL1 $TIME=2012/11:11:08:03:52
@CEU_SET_PARAMETER 4, HV_STEP_DWELL $TIME=2012/11:11:08:04:36
@CEU_SET_PARAMETER 16, HV_STEP_FRAC $TIME=2012/11:11:08:04:38
@CEU_LO_PMT_LVL 640 $TIME=2012/11:11:08:04:41
@CEU_SET_PARAMETER 1, HV_STEP_FRAC $TIME=2012/11:11:08:05:04
@CEU_LO_IF_PAC_VSET 5500 $TIME=2012/11:11:08:05:06
@CEU_LO_IF_MCP_VSET 2083 $TIME=2012/11:11:08:07:58
@CEU_SET_PARAMETER 11, HV_STEP_FRAC $TIME=2012/11:11:08:10:42
@CEU_LO_COL_NEG_LVL 216 $TIME=2012/11:11:08:10:44
@CEU_SET_PARAMETER 0, HV_STEP_DWELL $TIME=2012/11:11:08:12:00
@CEU_SET_PARAMETER 255, HV_STEP_FRAC $TIME=2012/11:11:08:12:02
@CEU_LO_U_POS_LVL 0 $TIME=2012/11:11:08:12:03
@CEU_LO_U_NEG_LVL 0 $TIME=2012/11:11:08:12:17
@CEU_SET_PARAMETER 4, HV_STEP_DWELL $TIME=2012/11:11:08:12:32
@CEU_SET_PARAMETER 1, HV_STEP_FRAC $TIME=2012/11:11:08:12:34
@CEU_MACRO_EXEC ASCENDING_PL2 $TIME=2012/11:11:08:12:56
# Orbit# 185 PERIGEE: Inertial MAneuver Commands
# @ECT_SetHTRCmd CATBED_5N_HTR,ON $TIME=2012/11:11:15:02:47
# @ACT_SetKFInputSelect GND_CMD, 0, 0, 0, 0 $TIME=2012/11:11:15:47:47
# @ACT_SetEstUpdateEnables ENABLE, DISABLE $TIME=2012/11:11:15:47:48
# @FCT_SetFcMode burn $TIME=2012/11:11:15:54:47
# @ACT_SetInrDir -0.679541,-0.667946,-0.303434 $TIME=2012/11:11:15:55:47
# @ACT_SetLrTarget ACS_INERTIAL $TIME=2012/11:11:15:56:47
# @ACT_SetThrustTime 660 $TIME=2012/11:11:15:57:42
# @ACT_SetThrustEnable ENABLE $TIME=2012/11:11:15:57:47
# @ACT_SetThrustEnable DISABLE $TIME=2012/11:11:16:07:47
# @ECT_SetHTRCmd CATBED_5N_HTR,OFF $TIME=2012/11:11:16:07:48
# @ACT_SetThrustTime 0 $TIME=2012/11:11:16:08:17
# @ACT_SetStaticZrate ESTIMATOR, 0.418 $TIME=2012/11:11:16:22:57
# @ACT_SetKFInputSelect STA_PCT_VALID, 48,18,23,53 $TIME=2012/11:11:16:23:07
# @FCT_SetFcMode Mission $TIME=2012/11:11:16:23:47
end
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Orbit# 185
IBEX,AUWA01,ADD,11/03/12,308,04:00:00,11/03/12,308,05:00:00,,LAHO 160K IBEX Orbit# 184 SSR_Dump/Tracking Contact (13 Asc)
IBEX,USHI01,ADD,11/08/12,313,09:00:00,11/08/12,313,09:35:00,,LAHO 2K IBEX Orbit#185 Apogee Contact (46 Desc)
IBEX,USAK01,ADD,11/11/12,316,12:00:00,11/11/12,316,13:00:00,,LAHO 160K IBEX Orbit# 185 SSR_Dump/Tracking Contact (12 Desc)
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