[Isocops] IBEX Orbit# 210 ATS (18 June 13 - 27 June 13)
Ibex Mission Operations
ibexops at gmail.com
Wed Jun 5 09:25:16 EDT 2013
Guys,
Here are the planning files and ATS for Orbit# 210. Please respond to
this email thread with all comments/approvals.
*Your comments/approvals are required before 8 June 13 @1300 UTC*
Note the following:
1. Hi negative collimator voltage set to 1400
2. Command Constraint Violations:
# IBEX_2013_169_o0210a_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
(304) 279-6678
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; Filename: IBEX_2013_169_o0210a_v001.scr
; File type: MAESTRO Absolute Time Sequence Script (ATS)
;
; Create time: 2013/156.102317
; Plan period start: 2013/169.174400
; Plan period stop: 2013/178.130500
; Default time format: UTC
;
; Input files: 4
; IBEX_2013_169_o0210a_v001.oef
; IBEX_2013_169_o0210a_v002.stf
; IBEX_2013_forecast_01jun13_21jul13_v001.sap
; IBEX_2013_Orbit210_v001.caf
; ATS_CMD_TIME_OFFSET = 0
script ats_2013_06_18_17_44_00()
begin
# Orbit# 210 Ascending BUS Commands
@ACT_SetSpinPulseProtectEnable Disable $TIME=2013/06:18:17:45:15
@FCT_SetScState science $TIME=2013/06:18:17:45:17
@ACT_SetSpinPulseProtectEnable Enable $TIME=2013/06:18:17:45:19
@CEU_LO_SCIENCE_MODE NORMAL $TIME=2013/06:18:17:45:21
# Orbit# 210 Ascending Payload Commands
# Hi negative collimator voltage set to 1400
@CEU_MACRO_EXEC ASCENDING_PL1 $TIME=2013/06:18:19:03:37
@CEU_MACRO_EXEC ASCENDING_HI $TIME=2013/06:18:19:03:53
@CEU_SET_PARAMETER 1, TLM_RATE_SOH $TIME=2013/06:18:19:14:55
@CEU_SET_PARAMETER 4, HV_STEP_DWELL $TIME=2013/06:18:19:14:58
@CEU_SET_PARAMETER 3, HV_STEP_FRAC $TIME=2013/06:18:19:15:02
@CEU_HI_COL_NEG_LVL 1400 $TIME=2013/06:18:19:15:06
@CEU_SET_PARAMETER 0, TLM_RATE_SOH $TIME=2013/06:18:19:15:41
@CEU_MACRO_EXEC ASCENDING_PL2 $TIME=2013/06:18:19:15:44
@CEU_MACRO_EXEC ASCENDING_PL1 $TIME=2013/06:18:19:17:49
@CEU_MACRO_EXEC ASCENDING_LO $TIME=2013/06:18:19:18:05
@CEU_MACRO_EXEC ASCENDING_PL2 $TIME=2013/06:18:19:26:25
# Orbit# 210 APOGEE: Descending Payload Commands
@CEU_MACRO_EXEC DESCENDING_PL1 $TIME=2013/06:22:05:10:07
@CEU_MACRO_EXEC DESCENDING_LO $TIME=2013/06:22:05:10:49
@CEU_MACRO_EXEC ASCENDING_PL2 $TIME=2013/06:22:05:19:11
@CEU_MACRO_EXEC DESCENDING_PL1 $TIME=2013/06:22:05:21:16
@CEU_MACRO_EXEC DESCENDING_HI $TIME=2013/06:22:05:21:58
@CEU_MACRO_EXEC DESCENDING_PL2 $TIME=2013/06:22:05:32:57
# Orbit# 210 APOGEE: Inertial Maneuver Commands
@FCT_SetScState housekeeping $TIME=2013/06:22:06:06:07
@ECT_SetHTRCmd CATBED_5N_HTR,ON $TIME=2013/06:22:06:11:05
@ACT_SetKFInputSelect GND_CMD, 0, 0, 0, 0 $TIME=2013/06:22:06:56:05
@ACT_SetEstUpdateEnables ENABLE, DISABLE $TIME=2013/06:22:06:56:06
@FCT_SetFcMode burn $TIME=2013/06:22:07:03:05
@ACT_SetInrDir 0.017609,0.921275,0.388513 $TIME=2013/06:22:07:04:05
@ACT_SetLrTarget ACS_INERTIAL $TIME=2013/06:22:07:05:05
@ACT_SetThrustTime 660 $TIME=2013/06:22:07:06:00
@ACT_SetThrustEnable ENABLE $TIME=2013/06:22:07:06:05
@ACT_SetThrustEnable DISABLE $TIME=2013/06:22:07:16:05
@ECT_SetHTRCmd CATBED_5N_HTR,OFF $TIME=2013/06:22:07:16:06
@ACT_SetThrustTime 0 $TIME=2013/06:22:07:16:35
@ACT_SetStaticZrate ESTIMATOR, 0.418 $TIME=2013/06:22:07:31:15
@ACT_SetKFInputSelect STA_PCT_VALID, 48,18,23,53 $TIME=2013/06:22:07:31:25
@FCT_SetFcMode Mission $TIME=2013/06:22:07:32:05
# Orbit# 210 APOGEE: Ascending BUS Commands
@ACT_SetSpinPulseProtectEnable Disable $TIME=2013/06:22:08:21:11
@FCT_SetScState science $TIME=2013/06:22:08:21:13
@ACT_SetSpinPulseProtectEnable Enable $TIME=2013/06:22:08:21:15
@CEU_LO_SCIENCE_MODE NORMAL $TIME=2013/06:22:08:21:17
# Orbit# 210 APOGEE: Ascending Payload Commands
# Hi negative collimator voltage set to 1400
@CEU_MACRO_EXEC ASCENDING_PL1 $TIME=2013/06:22:08:51:11
@CEU_MACRO_EXEC ASCENDING_HI $TIME=2013/06:22:08:51:27
@CEU_SET_PARAMETER 1, TLM_RATE_SOH $TIME=2013/06:22:09:02:29
@CEU_SET_PARAMETER 4, HV_STEP_DWELL $TIME=2013/06:22:09:02:32
@CEU_SET_PARAMETER 3, HV_STEP_FRAC $TIME=2013/06:22:09:02:36
@CEU_HI_COL_NEG_LVL 1400 $TIME=2013/06:22:09:02:40
@CEU_SET_PARAMETER 0, TLM_RATE_SOH $TIME=2013/06:22:09:03:15
@CEU_MACRO_EXEC ASCENDING_PL2 $TIME=2013/06:22:09:03:18
@CEU_MACRO_EXEC ASCENDING_PL1 $TIME=2013/06:22:09:05:23
@CEU_MACRO_EXEC ASCENDING_LO $TIME=2013/06:22:09:05:39
@CEU_MACRO_EXEC ASCENDING_PL2 $TIME=2013/06:22:09:13:59
# Orbit# 210 APOGEE: Apogee Contact
@ECT_SetRelay stx,on $TIME=2013/06:23:11:58:00
@FMI_SetDownlink2K $TIME=2013/06:23:11:58:02
@FMI_SetBilevelOutputControlReg STXMODE_Strobe,ON $TIME=2013/06:23:11:58:04
@FMI_SetBilevelOutputControlReg COHERENT,ON $TIME=2013/06:23:11:58:06
@ECT_SetRelay stx,off $TIME=2013/06:23:12:37:00
# Orbit# 210 PERIGEE: Descending Payload Commands
@CEU_MACRO_EXEC DESCENDING_PL1 $TIME=2013/06:26:14:02:24
@CEU_MACRO_EXEC DESCENDING_LO $TIME=2013/06:26:14:03:06
@CEU_MACRO_EXEC ASCENDING_PL2 $TIME=2013/06:26:14:11:28
@CEU_MACRO_EXEC DESCENDING_PL1 $TIME=2013/06:26:14:13:33
@CEU_MACRO_EXEC DESCENDING_HI $TIME=2013/06:26:14:14:15
@CEU_MACRO_EXEC DESCENDING_PL2 $TIME=2013/06:26:14:25:14
# Orbit# 210 PERIGEE: Inertial Maneuver Commands
@FCT_SetScState housekeeping $TIME=2013/06:26:15:14:30
@ECT_SetHTRCmd CATBED_5N_HTR,ON $TIME=2013/06:26:15:18:34
@ACT_SetKFInputSelect GND_CMD, 0, 0, 0, 0 $TIME=2013/06:26:16:03:34
@ACT_SetEstUpdateEnables ENABLE, DISABLE $TIME=2013/06:26:16:03:35
@FCT_SetFcMode burn $TIME=2013/06:26:16:10:34
@ACT_SetInrDir -0.056446,0.919984,0.38787 $TIME=2013/06:26:16:11:34
@ACT_SetLrTarget ACS_INERTIAL $TIME=2013/06:26:16:12:34
@ACT_SetThrustTime 660 $TIME=2013/06:26:16:13:29
@ACT_SetThrustEnable ENABLE $TIME=2013/06:26:16:13:34
@ACT_SetThrustEnable DISABLE $TIME=2013/06:26:16:23:34
@ECT_SetHTRCmd CATBED_5N_HTR,OFF $TIME=2013/06:26:16:23:35
@ACT_SetThrustTime 0 $TIME=2013/06:26:16:24:04
@ACT_SetStaticZrate ESTIMATOR, 0.418 $TIME=2013/06:26:16:38:44
@ACT_SetKFInputSelect STA_PCT_VALID, 48,18,23,53 $TIME=2013/06:26:16:38:54
@FCT_SetFcMode Mission $TIME=2013/06:26:16:39:34
# Orbit# 210 PERIGEE: SSR_Dump/Tracking Contact
@ECT_SetRelay stx,on $TIME=2013/06:26:20:58:00
@FMI_SetDownlink320K $TIME=2013/06:26:20:58:02
@FMI_SetBilevelOutputControlReg STXMODE_Strobe,ON $TIME=2013/06:26:20:58:04
@FMI_SetBilevelOutputControlReg COHERENT,ON $TIME=2013/06:26:20:58:06
@ECT_SetRelay stx,off $TIME=2013/06:26:22:02:00
# Orbit# 210 PERIGEE: Tracking Contact
@ECT_SetRelay stx,on $TIME=2013/06:27:08:58:00
@FMI_SetDownlink160K $TIME=2013/06:27:08:58:02
@FMI_SetBilevelOutputControlReg STXMODE_Strobe,ON $TIME=2013/06:27:08:58:04
@FMI_SetBilevelOutputControlReg COHERENT,ON $TIME=2013/06:27:08:58:06
@ECT_SetRelay stx,off $TIME=2013/06:27:09:37:00
end
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# Filename: IBEX_2013_169_o0210a_v001.ccvr
# File type: Command Load Constraint Violation Report (CCVR)
#
# Create time: 2013/156.102317
# Plan period start: 2013/169.174400
# Plan period stop: 2013/178.130500
# Default time format: UTC
#
# Input files: 1
# IBEX_2013_169_o0210a_v001.scr
==========================
HARD CONSTRAINT VIOLATIONS
==========================
NO VIOLATIONS.
==========================
SOFT CONSTRAINT VIOLATIONS
==========================
NO VIOLATIONS.
==============
OTHER MESSAGES
==============
NO MESSAGES.
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Orbit# 210
IBEX,USHI01,ADD,06/23/13,174,12:00:00,06/23/13,174,12:35:00,,LAHO 2K IBEX Orbit# 210 Apogee Contact (46 Desc)
IBEX,USAK01,ADD,06/26/13,177,21:00:00,06/26/13,177,22:00:00,,LAHO 320K IBEX Orbit# 210 SSR_Dump/Tracking Contact (10 Desc)
IBEX,USHI01,ADD,06/27/13,178,09:00:00,06/27/13,178,09:35:00,,LAHO 160K IBEX Orbit# 210 Tracking Contact (11 Asc)
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