[Isocops] Fwd: IBEX Orbit# 287 Hi Gain Test ATS (23 May 15)
Ibex Mission Operations
ibexops at gmail.com
Thu May 14 14:28:31 EDT 2015
---------- Forwarded message ----------
From: Ibex Mission Operations <ibexops at gmail.com>
Date: Tue, May 5, 2015 at 3:38 PM
Subject: IBEX Orbit# 287 Hi Gain Test ATS (23 May 15)
To: David Heirtzler <dheirtzl at atlas.sr.unh.edu>, IBEX FDG <
ibex at applieddefense.com>, ISOC at New Hampshire <isocops at lists.sr.unh.edu>,
Ken Fairchild <fair-play at comcast.net>, Marty Quinn <marty.quinn at unh.edu>,
Michelle Reno <mreno at swri.edu>, Nigel Angold <ngangold at earthlink.net>, Paul
Janzen <paul.janzen at umontana.edu>, Robert Lockwood <
robert.lockwood at orbitalatk.com>, Ryan Tyler <ryan.tyler at orbitalatk.com>,
Sheral Wesley <sheral.wesley at orbitalatk.com>, Tim Perry <
tim.perry at orbitalatk.com>
Here is the ATS for the IBEX_Hi Gain Test
Approvals will berequired before 21 May 15 @1200 UTC
--
Sheral R. Wesley
SPVR., Satellite Operations
IBEX Mission OPS
CYGNUS Mission Planning
(304) 279-6678
--
Sheral R. Wesley
SPVR., Satellite Operations
IBEX Mission OPS
CYGNUS Mission Planning
(304) 279-6678
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; Filename: IBEX_2015_139_o0287a_hgc_v001.scr
; File type: MAESTRO Absolute Time Sequence Script (ATS)
;
; Create time: 2015/125.142232
; Plan period start: 2015/139.194300
; Plan period stop: 2015/148.212500
; Default time format: UTC
;
; Input files: 2
; IBEX_2015_139_o0287a_v001.oef
; IBEX_2015_139_o0287a_v001_hgc.stf
; ATS_CMD_TIME_OFFSET = 0
script ats_2015_05_19_19_43_00()
begin
# Orbit# 287 APOGEE: Inertial MAneuver Commands
# @ECT_SetHTRCmd CATBED_5N_HTR,ON $TIME=2015/05:23:11:32:05
# @ACT_SetKFInputSelect GND_CMD, 0, 0, 0, 0 $TIME=2015/05:23:12:17:05
# @ACT_SetEstUpdateEnables ENABLE, DISABLE $TIME=2015/05:23:12:17:06
# @FCT_SetFcMode burn $TIME=2015/05:23:12:24:05
# @ACT_SetInrDir 0.499994,0.798574,0.33509 $TIME=2015/05:23:12:25:05
# @ACT_SetLrTarget ACS_INERTIAL $TIME=2015/05:23:12:26:05
# @ACT_SetThrustTime 660 $TIME=2015/05:23:12:27:00
# @ACT_SetThrustEnable ENABLE $TIME=2015/05:23:12:27:05
# @ACT_SetThrustEnable DISABLE $TIME=2015/05:23:12:37:05
# @ECT_SetHTRCmd CATBED_5N_HTR,OFF $TIME=2015/05:23:12:37:06
# @ACT_SetThrustTime 0 $TIME=2015/05:23:12:37:35
# @ACT_SetStaticZrate ESTIMATOR, 0.418 $TIME=2015/05:23:12:52:15
# @ACT_SetKFInputSelect STA_PCT_VALID, 48,18,23,53 $TIME=2015/05:23:12:52:25
# @FCT_SetFcMode Mission $TIME=2015/05:23:12:53:05
# Orbit# 287 APOGEE: IBEX_Hi Gain Test
@CEU_MODE HVENG $TIME=2015/05:26:02:00:00
@CEU_SET_PARAMETER 1,HV_STEP_DWELL $TIME=2015/05:26:02:00:36
@CEU_SET_PARAMETER 1,HV_STEP_FRAC $TIME=2015/05:26:02:00:38
@CEU_HI_TOF_BOX_LVL 5500 $TIME=2015/05:26:02:00:40
@CEU_HI_CEM_1_LVL 1860 $TIME=2015/05:26:02:01:19
@CEU_HI_CEM_2_LVL 1860 $TIME=2015/05:26:02:01:29
@CEU_HI_CEM_3_LVL 1860 $TIME=2015/05:26:02:01:39
@CEU_HI_CEM_4_LVL 1850 $TIME=2015/05:26:02:01:49
@CEU_MODE HVSCI $TIME=2015/05:26:02:02:39
@CEU_MODE HVENG $TIME=2015/05:26:02:27:59
@CEU_HI_CEM_1_LVL 1780 $TIME=2015/05:26:02:28:35
@CEU_HI_CEM_2_LVL 1780 $TIME=2015/05:26:02:28:45
@CEU_HI_CEM_3_LVL 1780 $TIME=2015/05:26:02:28:55
@CEU_HI_CEM_4_LVL 1900 $TIME=2015/05:26:02:29:05
@CEU_MODE HVSCI $TIME=2015/05:26:02:29:59
@CEU_MODE HVENG $TIME=2015/05:26:02:55:19
@CEU_HI_CEM_1_LVL 1600 $TIME=2015/05:26:02:55:55
@CEU_HI_CEM_2_LVL 1600 $TIME=2015/05:26:02:56:14
@CEU_HI_CEM_3_LVL 1600 $TIME=2015/05:26:02:56:33
@CEU_HI_CEM_4_LVL 1800 $TIME=2015/05:26:02:56:52
@CEU_MODE HVSCI $TIME=2015/05:26:02:57:51
@CEU_MODE HVENG $TIME=2015/05:26:03:23:11
@CEU_HI_CEM_1_LVL 1780 $TIME=2015/05:26:03:23:47
@CEU_HI_CEM_2_LVL 1780 $TIME=2015/05:26:03:24:06
@CEU_HI_CEM_3_LVL 1780 $TIME=2015/05:26:03:24:25
@CEU_HI_CEM_4_LVL 1900 $TIME=2015/05:26:03:24:44
@CEU_MODE HVSCI $TIME=2015/05:26:03:25:43
@CEU_MODE HVENG $TIME=2015/05:26:03:51:03
@CEU_HI_CEM_1_LVL 1500 $TIME=2015/05:26:03:51:39
@CEU_HI_CEM_2_LVL 1500 $TIME=2015/05:26:03:52:08
@CEU_HI_CEM_3_LVL 1500 $TIME=2015/05:26:03:52:37
@CEU_HI_CEM_4_LVL 1750 $TIME=2015/05:26:03:53:06
@CEU_MODE HVSCI $TIME=2015/05:26:03:54:15
@CEU_MODE HVENG $TIME=2015/05:26:04:19:35
@CEU_HI_CEM_1_LVL 1780 $TIME=2015/05:26:04:20:11
@CEU_HI_CEM_2_LVL 1780 $TIME=2015/05:26:04:20:40
@CEU_HI_CEM_3_LVL 1780 $TIME=2015/05:26:04:21:09
@CEU_HI_CEM_4_LVL 1900 $TIME=2015/05:26:04:21:38
@CEU_MODE HVSCI $TIME=2015/05:26:04:22:47
@CEU_MODE HVENG $TIME=2015/05:26:04:48:07
@CEU_HI_CEM_1_LVL 1400 $TIME=2015/05:26:04:48:43
@CEU_HI_CEM_2_LVL 1400 $TIME=2015/05:26:04:49:21
@CEU_HI_CEM_3_LVL 1400 $TIME=2015/05:26:04:49:59
@CEU_HI_CEM_4_LVL 1700 $TIME=2015/05:26:04:50:37
@CEU_MODE HVSCI $TIME=2015/05:26:04:51:55
@CEU_MODE HVENG $TIME=2015/05:26:05:17:15
@CEU_HI_CEM_1_LVL 1780 $TIME=2015/05:26:05:17:51
@CEU_HI_CEM_2_LVL 1780 $TIME=2015/05:26:05:18:29
@CEU_HI_CEM_3_LVL 1780 $TIME=2015/05:26:05:19:07
@CEU_HI_CEM_4_LVL 1900 $TIME=2015/05:26:05:19:45
@CEU_MODE HVSCI $TIME=2015/05:26:05:21:03
@CEU_MODE HVENG $TIME=2015/05:26:05:46:23
@CEU_HI_CEM_1_LVL 1700 $TIME=2015/05:26:05:46:59
@CEU_HI_CEM_2_LVL 1700 $TIME=2015/05:26:05:47:09
@CEU_HI_CEM_3_LVL 1700 $TIME=2015/05:26:05:47:19
@CEU_HI_CEM_4_LVL 1850 $TIME=2015/05:26:05:47:29
@CEU_MODE HVSCI $TIME=2015/05:26:05:48:23
@CEU_MODE HVENG $TIME=2015/05:26:06:13:41
@CEU_HI_CEM_1_LVL 1780 $TIME=2015/05:26:06:14:17
@CEU_HI_CEM_2_LVL 1780 $TIME=2015/05:26:06:14:27
@CEU_HI_CEM_3_LVL 1780 $TIME=2015/05:26:06:14:37
@CEU_HI_CEM_4_LVL 1900 $TIME=2015/05:26:06:14:47
@CEU_HI_TOF_BOX_LVL 6000 $TIME=2015/05:26:06:14:57
@CEU_MODE HVSCI $TIME=2015/05:26:06:15:41
# Orbit# 287 PERIGEE: Inertial Maneuver Commands
# @ECT_SetHTRCmd CATBED_5N_HTR,ON $TIME=2015/05:28:05:35:25
# @ACT_SetKFInputSelect GND_CMD, 0, 0, 0, 0 $TIME=2015/05:28:06:20:25
# @ACT_SetEstUpdateEnables ENABLE, DISABLE $TIME=2015/05:28:06:20:26
# @FCT_SetFcMode burn $TIME=2015/05:28:06:27:25
# @ACT_SetInrDir 0.431959,0.831344,0.349684 $TIME=2015/05:28:06:28:25
# @ACT_SetLrTarget ACS_INERTIAL $TIME=2015/05:28:06:29:25
# @ACT_SetThrustTime 660 $TIME=2015/05:28:06:30:20
# @ACT_SetThrustEnable ENABLE $TIME=2015/05:28:06:30:25
# @ACT_SetThrustEnable DISABLE $TIME=2015/05:28:06:40:25
# @ECT_SetHTRCmd CATBED_5N_HTR,OFF $TIME=2015/05:28:06:40:26
# @ACT_SetThrustTime 0 $TIME=2015/05:28:06:40:55
# @ACT_SetStaticZrate ESTIMATOR, 0.418 $TIME=2015/05:28:06:55:35
# @ACT_SetKFInputSelect STA_PCT_VALID, 48,18,23,53 $TIME=2015/05:28:06:55:45
# @FCT_SetFcMode Mission $TIME=2015/05:28:06:56:25
end
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