[Isocops] IBEX Orbit# 251 ATS (26 Jun14 - 5 Jul 14)
Ibex Mission Operations
ibexops at gmail.com
Fri Jun 13 07:56:46 EDT 2014
Guys,
Here are the planning files and ATS for Orbit# 251.
Please respond to this email thread with questions and approvals.
*Approvals are required before 16 June 14 @1800 UTC*
Note the following:
1. Battery Balancing at Perigee
ECT_SetLongEclipseFlag TRUE $TIME=2014/07:05:23:00:00
ECT_SetLongEclipseFlag FALSE $TIME=2014/07:06:00:30:00
2. Moon in Lo FOV
Moon in LO FOV Commands
# 2014-07-04T08:56:43.538Z,MoonInLoFovStart,orbit:251
# 2014-07-04T12:39:11.923Z,MoonInLoFovStop,orbit:251
# 2014-07-04T14:55:38.908Z,MoonInLoFovStart,orbit:251
# 2014-07-05T05:59:15.482Z,MoonInLoFovStop,orbit:251
3. New Payload Voltage settings
Special Ops/Post-LUT Changes
# CCB Description
# 2013-05-15 Hi negative collimator voltage set to 1400
# 2014-05-28 Hi CEMs A-C set to 1780, CEM D set to 1900
4. Command Load Constraint Violation Report (CCVR)
# IBEX_2014_177_o0251a_v001.scr
==========================
HARD CONSTRAINT VIOLATIONS
==========================
NO VIOLATIONS.
==========================
SOFT CONSTRAINT VIOLATIONS
==========================
NO VIOLATIONS.
==============
OTHER MESSAGES
==============
NO MESSAGES.
--
Sheral R. Wesley
SPVR., Satellite Operations
IBEX Mission OPS
CYGNUS Mission Planning
(304) 279-6678
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; Filename: IBEX_2014_177_o0251a_v001.scr
; File type: MAESTRO Absolute Time Sequence Script (ATS)
;
; Create time: 2014/164.112550
; Plan period start: 2014/178.015900
; Plan period stop: 2014/187.095900
; Default time format: UTC
;
; Input files: 4
; IBEX_2014_177_o0251a_v001.oef
; IBEX_2014_177_o0251a_v002.stf
; IBEX_2014_forecast_08jun14_27jul14_v001.sap
; IBEX_2014_Orbit251_v001.caf
; ATS_CMD_TIME_OFFSET = 0
script ats_2014_06_27_01_59_00()
begin
# Orbit# 251 Ascending BUS Commands
@ACT_SetSpinPulseProtectEnable Disable $TIME=2014/06:27:02:00:13
@FCT_SetScState science $TIME=2014/06:27:02:00:15
@ACT_SetSpinPulseProtectEnable Enable $TIME=2014/06:27:02:00:17
@CEU_LO_SCIENCE_MODE NORMAL $TIME=2014/06:27:02:00:19
# Orbit# 251 Ascending Payload Commands
# Hi CEMs A-C set to 1780, CEM D set to 1900
@CEU_MACRO_EXEC ASCENDING_PL1 $TIME=2014/06:27:03:29:30
@CEU_MACRO_EXEC ASCENDING_HI $TIME=2014/06:27:03:29:46
@CEU_SET_PARAMETER 1, TLM_RATE_SOH $TIME=2014/06:27:03:40:48
@CEU_SET_PARAMETER 4, HV_STEP_DWELL $TIME=2014/06:27:03:40:51
@CEU_SET_PARAMETER 3, HV_STEP_FRAC $TIME=2014/06:27:03:40:55
@CEU_HI_COL_NEG_LVL 1400 $TIME=2014/06:27:03:40:59
@CEU_HI_CEM_1_LVL 1780 $TIME=2014/06:27:03:41:34
@CEU_HI_CEM_2_LVL 1780 $TIME=2014/06:27:03:41:49
@CEU_HI_CEM_3_LVL 1780 $TIME=2014/06:27:03:42:04
@CEU_HI_CEM_4_LVL 1900 $TIME=2014/06:27:03:42:19
@CEU_SET_PARAMETER 0, TLM_RATE_SOH $TIME=2014/06:27:03:42:34
@CEU_MACRO_EXEC ASCENDING_PL2 $TIME=2014/06:27:03:42:37
@CEU_MACRO_EXEC ASCENDING_PL1 $TIME=2014/06:27:03:44:42
@CEU_MACRO_EXEC ASCENDING_LO $TIME=2014/06:27:03:44:58
@CEU_MACRO_EXEC ASCENDING_PL2 $TIME=2014/06:27:03:53:18
# Orbit# 251 APOGEE: Descending Payload Commands
@CEU_MACRO_EXEC DESCENDING_PL1 $TIME=2014/06:30:19:55:06
@CEU_MACRO_EXEC DESCENDING_LO $TIME=2014/06:30:19:55:48
@CEU_MACRO_EXEC ASCENDING_PL2 $TIME=2014/06:30:20:04:10
@CEU_MACRO_EXEC DESCENDING_PL1 $TIME=2014/06:30:20:06:15
@CEU_MACRO_EXEC DESCENDING_HI $TIME=2014/06:30:20:06:57
@CEU_MACRO_EXEC DESCENDING_PL2 $TIME=2014/06:30:20:17:56
# Orbit# 251 APOGEE: Inertial MAneuver Commands
@FCT_SetScState housekeeping $TIME=2014/06:30:20:51:06
@ECT_SetHTRCmd CATBED_5N_HTR,ON $TIME=2014/06:30:20:56:04
@ACT_SetKFInputSelect GND_CMD, 0, 0, 0, 0 $TIME=2014/06:30:21:41:04
@ACT_SetEstUpdateEnables ENABLE, DISABLE $TIME=2014/06:30:21:41:05
@FCT_SetFcMode burn $TIME=2014/06:30:21:48:04
@ACT_SetInrDir -0.120898,0.914731,0.385552 $TIME=2014/06:30:21:49:04
@ACT_SetLrTarget ACS_INERTIAL $TIME=2014/06:30:21:50:04
@ACT_SetThrustTime 660 $TIME=2014/06:30:21:50:59
@ACT_SetThrustEnable ENABLE $TIME=2014/06:30:21:51:04
@ACT_SetThrustEnable DISABLE $TIME=2014/06:30:22:01:04
@ECT_SetHTRCmd CATBED_5N_HTR,OFF $TIME=2014/06:30:22:01:05
@ACT_SetThrustTime 0 $TIME=2014/06:30:22:01:34
@ACT_SetStaticZrate ESTIMATOR, 0.418 $TIME=2014/06:30:22:16:14
@ACT_SetKFInputSelect STA_PCT_VALID, 48,18,23,53 $TIME=2014/06:30:22:16:24
@FCT_SetFcMode Mission $TIME=2014/06:30:22:17:04
# Orbit# 251 APOGEE: Ascending BUS Commands
@ACT_SetSpinPulseProtectEnable Disable $TIME=2014/06:30:23:06:10
@FCT_SetScState science $TIME=2014/06:30:23:06:12
@ACT_SetSpinPulseProtectEnable Enable $TIME=2014/06:30:23:06:14
@CEU_LO_SCIENCE_MODE NORMAL $TIME=2014/06:30:23:06:16
# Orbit# 251 APOGEE: Ascending Payload Commands
# Hi CEMs A-C set to 1780, CEM D set to 1900
@CEU_MACRO_EXEC ASCENDING_PL1 $TIME=2014/06:30:23:36:10
@CEU_MACRO_EXEC ASCENDING_HI $TIME=2014/06:30:23:36:26
@CEU_SET_PARAMETER 1, TLM_RATE_SOH $TIME=2014/06:30:23:47:28
@CEU_SET_PARAMETER 4, HV_STEP_DWELL $TIME=2014/06:30:23:47:31
@CEU_SET_PARAMETER 3, HV_STEP_FRAC $TIME=2014/06:30:23:47:35
@CEU_HI_COL_NEG_LVL 1400 $TIME=2014/06:30:23:47:39
@CEU_HI_CEM_1_LVL 1780 $TIME=2014/06:30:23:48:14
@CEU_HI_CEM_2_LVL 1780 $TIME=2014/06:30:23:48:29
@CEU_HI_CEM_3_LVL 1780 $TIME=2014/06:30:23:48:44
@CEU_HI_CEM_4_LVL 1900 $TIME=2014/06:30:23:48:59
@CEU_SET_PARAMETER 0, TLM_RATE_SOH $TIME=2014/06:30:23:49:14
@CEU_MACRO_EXEC ASCENDING_PL2 $TIME=2014/06:30:23:49:17
@CEU_MACRO_EXEC ASCENDING_PL1 $TIME=2014/06:30:23:51:22
@CEU_MACRO_EXEC ASCENDING_LO $TIME=2014/06:30:23:51:38
@CEU_MACRO_EXEC ASCENDING_PL2 $TIME=2014/06:30:23:59:58
# Orbit# 251 APOGEE: Apogee Tracking Contact
@ECT_SetRelay stx,on $TIME=2014/07:01:15:58:00
@FMI_SetDownlink2K $TIME=2014/07:01:15:58:02
@FMI_SetBilevelOutputControlReg STXMODE_Strobe,ON $TIME=2014/07:01:15:58:04
@FMI_SetBilevelOutputControlReg COHERENT,ON $TIME=2014/07:01:15:58:06
@ECT_SetRelay stx,off $TIME=2014/07:01:16:37:00
# Orbit# 251 APOGEE: Moon in LO FOV Commands
# 2014-07-04T08:56:43.538Z,MoonInLoFovStart,orbit:251
# 2014-07-04T12:39:11.923Z,MoonInLoFovStop,orbit:251
# 2014-07-04T14:55:38.908Z,MoonInLoFovStart,orbit:251
# 2014-07-05T05:59:15.482Z,MoonInLoFovStop,orbit:251
@CEU_LO_PMT_LVL 300 $TIME=2014/07:04:10:15:00
@CEU_LO_IF_STAR_ADJ 0 $TIME=2014/07:04:10:15:02
@CEU_LO_IF_STAR_ADJ 250 $TIME=2014/07:05:03:31:58
@CEU_LO_PMT_LVL 800 $TIME=2014/07:05:03:32:00
# Orbit# 251 PERIGEE: Descending Payload Commands
@CEU_MACRO_EXEC DESCENDING_PL1 $TIME=2014/07:05:11:24:06
@CEU_MACRO_EXEC DESCENDING_LO $TIME=2014/07:05:11:24:48
@CEU_MACRO_EXEC ASCENDING_PL2 $TIME=2014/07:05:11:33:10
@CEU_MACRO_EXEC DESCENDING_PL1 $TIME=2014/07:05:11:35:15
@CEU_MACRO_EXEC DESCENDING_HI $TIME=2014/07:05:11:35:57
@CEU_MACRO_EXEC DESCENDING_PL2 $TIME=2014/07:05:11:46:56
# Orbit# 251 PERIGEE: Inertial Maneuver Commands
@FCT_SetScState housekeeping $TIME=2014/07:05:12:48:15
@ECT_SetHTRCmd CATBED_5N_HTR,ON $TIME=2014/07:05:12:51:53
@ACT_SetKFInputSelect GND_CMD, 0, 0, 0, 0 $TIME=2014/07:05:13:36:53
@ACT_SetEstUpdateEnables ENABLE, DISABLE $TIME=2014/07:05:13:36:54
@FCT_SetFcMode burn $TIME=2014/07:05:13:43:53
@ACT_SetInrDir -0.198723,0.903093,0.380699 $TIME=2014/07:05:13:44:53
@ACT_SetLrTarget ACS_INERTIAL $TIME=2014/07:05:13:45:53
@ACT_SetThrustTime 660 $TIME=2014/07:05:13:46:48
@ACT_SetThrustEnable ENABLE $TIME=2014/07:05:13:46:53
@ACT_SetThrustEnable DISABLE $TIME=2014/07:05:13:56:53
@ECT_SetHTRCmd CATBED_5N_HTR,OFF $TIME=2014/07:05:13:56:54
@ACT_SetThrustTime 0 $TIME=2014/07:05:13:57:23
@ACT_SetStaticZrate ESTIMATOR, 0.418 $TIME=2014/07:05:14:12:03
@ACT_SetKFInputSelect STA_PCT_VALID, 48,18,23,53 $TIME=2014/07:05:14:12:13
@FCT_SetFcMode Mission $TIME=2014/07:05:14:12:53
# Orbit# 251 PERIGEE: Tracking Contact 05 July 14 @1800-1835 UTC
# Orbit# 251 PERIGEE: Battery Balancing Commands
@ECT_SetLongEclipseFlag TRUE $TIME=2014/07:05:23:00:00
@ECT_SetLongEclipseFlag FALSE $TIME=2014/07:06:00:30:00
# Orbit# 251 PERIGEE: SSR_Dump/Tracking Contact 06 July 14 @0800-0900 UTC
end
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# Filename: IBEX_2014_177_o0251a_v001.ccvr
# File type: Command Load Constraint Violation Report (CCVR)
#
# Create time: 2014/164.112550
# Plan period start: 2014/178.015900
# Plan period stop: 2014/187.095900
# Default time format: UTC
#
# Input files: 1
# IBEX_2014_177_o0251a_v001.scr
==========================
HARD CONSTRAINT VIOLATIONS
==========================
NO VIOLATIONS.
==========================
SOFT CONSTRAINT VIOLATIONS
==========================
NO VIOLATIONS.
==============
OTHER MESSAGES
==============
NO MESSAGES.
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Orbit# 251
IBEX,USHI01,ADD,07/01/14,182,16:00:00,07/01/14,182,16:35:00,,LAHO 2K IBEX Orbit# 251 Apogee Contact (47 Desc)
IBEX,USAK01,ADD,07/05/14,186,18:00:00,07/05/14,186,18:35:00,,LAHO 40K IBEX Orbit# 251 Tracking Contact (11 Desc)
IBEX,USHI01,ADD,07/06/14,187,08:00:00,07/06/14,187,09:00:00,,LAHO 160K IBEX Orbit# 251 SSR_Dump/Tracking Contact (13 Asc)
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