[Isocops] IBEX Orbit# 240 ATS (17 Mar 14 - 26 Mar 14)
Ibex Mission Operations
ibexops at gmail.com
Tue Mar 4 14:51:18 EST 2014
Guys,
Here are the planning files for Orbit# 240.
Please respond to this email thread with any questions and approvals.
All approvals are required before 7 Mar 14 @2200 UTC
Please note the following
1. OEF Generation
The OEF was generated using o0238a OEF because Orbit# 239 has a Sun
Maneuver at Perigee
2. Small Eclipse at Perigee that requires no action
# Orbit# 240 PERIGEE: Small Eclipse, No Action Required
# 2014-03-26T10:26:50.562Z,EclipseEntry,moderate:false,long:false,orbit:240
# 2014-03-26T10:42:37.825Z,EclipseExit,moderate:false,long:false,orbit:240
3. No Battery Balancing Commands
4. Moon in Lo FOV Commands
# Orbit# 240 APOGEE: Moon in Lo FOV Commands
# 2014-03-25T00:30:09.041Z,MoonInLoFovStart,orbit:240
# 2014-03-25T12:51:01.535Z,MoonInLoFovStop,orbit:240
5. IBEX_Hi Gain Test commands occur around Apogee commands
# Orbit# 240 IBEX_Hi Gain Test
# Start: $TIME=2014/03:19:16:00:00
# End: $TIME=2014/03:19:20:13:45
6. Special Ops/Post-LUT Changes
Hi negative collimator voltage set to 1400
Hi ABAB (CEM comparison)
--
Sheral R. Wesley
SPVR., Satellite Operations
IBEX Mission OPS
CYGNUS Mission Planning
(304) 279-6678
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; Filename: IBEX_2014_076_o0240a_v001.scr
; File type: MAESTRO Absolute Time Sequence Script (ATS)
;
; Create time: 2014/063.175841
; Plan period start: 2014/076.170500
; Plan period stop: 2014/085.161700
; Default time format: UTC
;
; Input files: 4
; IBEX_2014_076_o0240a_v001.oef
; IBEX_2014_076_o0240a_v003.stf
; IBEX_2014_forecast_27feb14_17apr14_v001.sap
; IBEX_2014_Orbit240_v001.caf
; ATS_CMD_TIME_OFFSET = 0
script ats_2014_03_17_17_05_00()
begin
# Orbit# 240 Ascending BUS Commands
@ACT_SetSpinPulseProtectEnable Disable $TIME=2014/03:17:17:05:08
@FCT_SetScState science $TIME=2014/03:17:17:05:10
@ACT_SetSpinPulseProtectEnable Enable $TIME=2014/03:17:17:05:12
@CEU_LO_SCIENCE_MODE NORMAL $TIME=2014/03:17:17:05:14
# Orbit# 240 Ascending PAyload Commands
@CEU_MACRO_EXEC ASCENDING_PL1 $TIME=2014/03:17:18:26:06
@CEU_MACRO_EXEC ASCENDING_HI $TIME=2014/03:17:18:26:22
@CEU_SET_PARAMETER 1, TLM_RATE_SOH $TIME=2014/03:17:18:37:24
@CEU_SET_PARAMETER 4, HV_STEP_DWELL $TIME=2014/03:17:18:37:27
@CEU_SET_PARAMETER 3, HV_STEP_FRAC $TIME=2014/03:17:18:37:31
@CEU_HI_COL_NEG_LVL 1400 $TIME=2014/03:17:18:37:35
@CEU_SET_PARAMETER 0, TLM_RATE_SOH $TIME=2014/03:17:18:38:10
@CEU_MACRO_EXEC ASCENDING_PL2 $TIME=2014/03:17:18:38:13
@CEU_MACRO_EXEC ASCENDING_PL1 $TIME=2014/03:17:18:40:18
@CEU_MACRO_EXEC ASCENDING_LO $TIME=2014/03:17:18:40:34
@CEU_MACRO_EXEC ASCENDING_PL2 $TIME=2014/03:17:18:48:54
# Orbit# 240 APOGEE: IBEX_ Hi ABAB (CEM comparison) Commands
@CEU_MODE HVENG $TIME=2014/03:18:16:41:02
@CEU_HI_CEM_1_LVL 1780 $TIME=2014/03:18:16:41:40
@CEU_HI_CEM_2_LVL 1780 $TIME=2014/03:18:16:42:10
@CEU_HI_CEM_3_LVL 1780 $TIME=2014/03:18:16:42:40
@CEU_MODE HVSCI $TIME=2014/03:18:16:43:10
@CEU_MODE HVENG $TIME=2014/03:19:14:31:03
@CEU_HI_CEM_1_LVL 1700 $TIME=2014/03:19:14:31:41
@CEU_HI_CEM_2_LVL 1700 $TIME=2014/03:19:14:32:11
@CEU_HI_CEM_3_LVL 1700 $TIME=2014/03:19:14:32:41
@CEU_MODE HVSCI $TIME=2014/03:19:14:33:11
# Orbit# 240 IBEX_Hi Gain Test
# Start: $TIME=2014/03:19:16:00:00
# End: $TIME=2014/03:19:20:13:45
# Orbit# 240 APOGEE: IBEX_Hi ABAB (CEM comparison )Commands
@CEU_MODE HVENG $TIME=2014/03:20:12:21:04
@CEU_HI_CEM_1_LVL 1780 $TIME=2014/03:20:12:21:42
@CEU_HI_CEM_2_LVL 1780 $TIME=2014/03:20:12:22:12
@CEU_HI_CEM_3_LVL 1780 $TIME=2014/03:20:12:22:42
@CEU_MODE HVSCI $TIME=2014/03:20:12:23:12
# Orbit# 240 APOGEE: Descending PAyload Commands
@CEU_MACRO_EXEC DESCENDING_PL1 $TIME=2014/03:21:10:11:08
@CEU_MACRO_EXEC DESCENDING_LO $TIME=2014/03:21:10:11:50
@CEU_MACRO_EXEC ASCENDING_PL2 $TIME=2014/03:21:10:20:12
@CEU_MACRO_EXEC DESCENDING_PL1 $TIME=2014/03:21:10:22:17
@CEU_MACRO_EXEC DESCENDING_HI $TIME=2014/03:21:10:22:59
@CEU_MACRO_EXEC DESCENDING_PL2 $TIME=2014/03:21:10:33:58
# Orbit# 240 APOGEE: Inertial Maneuver Commands
@FCT_SetScState housekeeping $TIME=2014/03:21:11:07:08
@ECT_SetHTRCmd CATBED_5N_HTR,ON $TIME=2014/03:21:11:12:28
@ACT_SetKFInputSelect GND_CMD, 0, 0, 0, 0 $TIME=2014/03:21:11:57:28
@ACT_SetEstUpdateEnables ENABLE, DISABLE $TIME=2014/03:21:11:57:29
@FCT_SetFcMode burn $TIME=2014/03:21:12:04:28
@ACT_SetInrDir 0.999618,-0.019613,-0.019494 $TIME=2014/03:21:12:05:28
@ACT_SetLrTarget ACS_INERTIAL $TIME=2014/03:21:12:06:28
@ACT_SetThrustTime 660 $TIME=2014/03:21:12:07:23
@ACT_SetThrustEnable ENABLE $TIME=2014/03:21:12:07:28
@ACT_SetThrustEnable DISABLE $TIME=2014/03:21:12:17:28
@ECT_SetHTRCmd CATBED_5N_HTR,OFF $TIME=2014/03:21:12:17:29
@ACT_SetThrustTime 0 $TIME=2014/03:21:12:17:58
@ACT_SetStaticZrate ESTIMATOR, 0.418 $TIME=2014/03:21:12:32:38
@ACT_SetKFInputSelect STA_PCT_VALID, 48,18,23,53 $TIME=2014/03:21:12:32:48
@FCT_SetFcMode Mission $TIME=2014/03:21:12:33:28
# Orbit# 240 APOGEE: Ascending BUS Commands
@ACT_SetSpinPulseProtectEnable Disable $TIME=2014/03:21:13:22:12
@FCT_SetScState science $TIME=2014/03:21:13:22:14
@ACT_SetSpinPulseProtectEnable Enable $TIME=2014/03:21:13:22:16
@CEU_LO_SCIENCE_MODE NORMAL $TIME=2014/03:21:13:22:18
# Orbit# 240 APOGEE: Ascending Payload Commands
@CEU_MACRO_EXEC ASCENDING_PL1 $TIME=2014/03:21:13:52:12
@CEU_MACRO_EXEC ASCENDING_HI $TIME=2014/03:21:13:52:28
@CEU_SET_PARAMETER 1, TLM_RATE_SOH $TIME=2014/03:21:14:03:30
@CEU_SET_PARAMETER 4, HV_STEP_DWELL $TIME=2014/03:21:14:03:33
@CEU_SET_PARAMETER 3, HV_STEP_FRAC $TIME=2014/03:21:14:03:37
@CEU_HI_COL_NEG_LVL 1400 $TIME=2014/03:21:14:03:41
@CEU_SET_PARAMETER 0, TLM_RATE_SOH $TIME=2014/03:21:14:04:16
@CEU_MACRO_EXEC ASCENDING_PL2 $TIME=2014/03:21:14:04:19
@CEU_MACRO_EXEC ASCENDING_PL1 $TIME=2014/03:21:14:06:24
@CEU_MACRO_EXEC ASCENDING_LO $TIME=2014/03:21:14:06:40
@CEU_MACRO_EXEC ASCENDING_PL2 $TIME=2014/03:21:14:15:00
# Orbit# 240 APOGEE: IBEX_Hi ABAB (CEM comparison )Commands
@CEU_MODE HVENG $TIME=2014/03:22:15:03:47
@CEU_HI_CEM_1_LVL 1780 $TIME=2014/03:22:15:04:25
@CEU_HI_CEM_2_LVL 1780 $TIME=2014/03:22:15:04:55
@CEU_HI_CEM_3_LVL 1780 $TIME=2014/03:22:15:05:25
@CEU_MODE HVSCI $TIME=2014/03:22:15:05:55
# Orbit# 240 APOGEE: Apogee Contact Commands
@ECT_SetRelay stx,on $TIME=2014/03:22:15:58:00
@FMI_SetDownlink2K $TIME=2014/03:22:15:58:02
@FMI_SetBilevelOutputControlReg STXMODE_Strobe,ON $TIME=2014/03:22:15:58:04
@FMI_SetBilevelOutputControlReg COHERENT,ON $TIME=2014/03:22:15:58:06
@ECT_SetRelay stx,off $TIME=2014/03:22:16:37:00
# Orbit# 240 APOGEE: IBEX_Hi ABAB (CEM comparison )Commands
@CEU_MODE HVENG $TIME=2014/03:23:15:50:27
@CEU_HI_CEM_1_LVL 1700 $TIME=2014/03:23:15:51:05
@CEU_HI_CEM_2_LVL 1700 $TIME=2014/03:23:15:51:35
@CEU_HI_CEM_3_LVL 1700 $TIME=2014/03:23:15:52:05
@CEU_MODE HVSCI $TIME=2014/03:23:15:52:35
@CEU_MODE HVENG $TIME=2014/03:24:16:37:07
@CEU_HI_CEM_1_LVL 1780 $TIME=2014/03:24:16:37:45
@CEU_HI_CEM_2_LVL 1780 $TIME=2014/03:24:16:38:15
@CEU_HI_CEM_3_LVL 1780 $TIME=2014/03:24:16:38:45
@CEU_MODE HVSCI $TIME=2014/03:24:16:39:15
# Orbit# 240 APOGEE: Moon in Lo FOV Commands
# 2014-03-25T00:30:09.041Z,MoonInLoFovStart,orbit:240
# 2014-03-25T12:51:01.535Z,MoonInLoFovStop,orbit:240
@CEU_LO_PMT_LVL 300 $TIME=2014/03:25:01:13:44
@CEU_LO_IF_STAR_ADJ 0 $TIME=2014/03:25:01:13:46
@CEU_LO_IF_STAR_ADJ 250 $TIME=2014/03:25:11:19:27
@CEU_LO_PMT_LVL 800 $TIME=2014/03:25:11:19:29
# Orbit# 240 PERIGEE: Descending Payload Commands
@CEU_MACRO_EXEC DESCENDING_PL1 $TIME=2014/03:25:17:23:49
@CEU_MACRO_EXEC DESCENDING_LO $TIME=2014/03:25:17:24:31
@CEU_MACRO_EXEC ASCENDING_PL2 $TIME=2014/03:25:17:32:53
@CEU_MACRO_EXEC DESCENDING_PL1 $TIME=2014/03:25:17:34:58
@CEU_MACRO_EXEC DESCENDING_HI $TIME=2014/03:25:17:35:40
@CEU_MACRO_EXEC DESCENDING_PL2 $TIME=2014/03:25:17:46:39
# Orbit# 240 PERIGEE: Inertial Maneuver Commands
@FCT_SetScState housekeeping $TIME=2014/03:25:18:43:47
@ECT_SetHTRCmd CATBED_5N_HTR,ON $TIME=2014/03:25:18:46:41
@ACT_SetKFInputSelect GND_CMD, 0, 0, 0, 0 $TIME=2014/03:25:19:31:41
@ACT_SetEstUpdateEnables ENABLE, DISABLE $TIME=2014/03:25:19:31:42
@FCT_SetFcMode burn $TIME=2014/03:25:19:38:41
@ACT_SetInrDir 0.998634,0.051025,0.011292 $TIME=2014/03:25:19:39:41
@ACT_SetLrTarget ACS_INERTIAL $TIME=2014/03:25:19:40:41
@ACT_SetThrustTime 660 $TIME=2014/03:25:19:41:36
@ACT_SetThrustEnable ENABLE $TIME=2014/03:25:19:41:41
@ACT_SetThrustEnable DISABLE $TIME=2014/03:25:19:51:41
@ECT_SetHTRCmd CATBED_5N_HTR,OFF $TIME=2014/03:25:19:51:42
@ACT_SetThrustTime 0 $TIME=2014/03:25:19:52:11
@ACT_SetStaticZrate ESTIMATOR, 0.418 $TIME=2014/03:25:20:06:51
@ACT_SetKFInputSelect STA_PCT_VALID, 48,18,23,53 $TIME=2014/03:25:20:07:01
@FCT_SetFcMode Mission $TIME=2014/03:25:20:07:41
# Orbit# 240 PERIGEE: Small Eclipse, No Action Required
# 2014-03-26T10:26:50.562Z,EclipseEntry,moderate:false,long:false,orbit:240
# 2014-03-26T10:42:37.825Z,EclipseExit,moderate:false,long:false,orbit:240
end
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# Filename: IBEX_2014_076_o0240a_v001.ccvr
# File type: Command Load Constraint Violation Report (CCVR)
#
# Create time: 2014/063.175841
# Plan period start: 2014/076.170500
# Plan period stop: 2014/085.161700
# Default time format: UTC
#
# Input files: 1
# IBEX_2014_076_o0240a_v001.scr
==========================
HARD CONSTRAINT VIOLATIONS
==========================
NO VIOLATIONS.
==========================
SOFT CONSTRAINT VIOLATIONS
==========================
NO VIOLATIONS.
==============
OTHER MESSAGES
==============
NO MESSAGES.
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Orbit# 240
IBEX,USHI01,ADD,03/22/14,081,16:00:00,03/22/14,081,16:35:00,,LAHO 2K IBEX Orbit# 240 Apogee Contact (Apogee)
IBEX,USHI01,ADD,03/26/14,085,00:00:00,03/26/14,085,01:00:00,,LAHO 160K IBEX ORbit# 240 SSR_Dump/Tracking Contact(11 Desc)
* Back-Up Star Tracker Image Dump Contact*
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