[Isocops] IBEX Orbit# 155 Recovery ATS files
Ibex Mission Operations
ibexops at gmail.com
Thu Feb 9 09:55:50 EST 2012
Guys,
I have included V002 of the contact ATS and the Sun Precession MAneuver
On Thu, Feb 9, 2012 at 9:37 AM, Ibex Mission Operations
<ibexops at gmail.com>wrote:
> Guys,
> Here are the ATS files for Recovery.
>
> *1. IBEX_2012_Recovery_NoOMODE_v001.scr
> *Does not contain PERIGEE OMODE commands
>
> *2. IBEX_2012_Recovery_OMODE_v001.scr
> *Contains PERIGEE OMODE commands from the Orbit# 155 ATS
>
> *3. IBEX_2012_034_o0155a_old_v001.scr*
> A refrernce of the ATS command load for Orbit# 155
>
> *4. IBEX_2012_Orbit155_RecoveryContacts_v001.scr*
> Contacts scheduled for recovery operations on USN/HAW02
>
> IBEX,USHI02,ADD,02/09/12,040,19:00:00,02/09/12,040,20:00:00,,LAHO 2K
> Orbit# 155 BUS Recovery
> IBEX,USHI02,ADD,02/09/12,040,21:30:00,02/09/12,040,23:00:00,,LAHO 2K
> Orbit# 155 Payload Recovery
> IBEX,USHI02,ADD,02/10/12,041,00:00:00,02/10/12,041,01:00:00,,LAHO 2K
> Orbit# 155 Payload Recovery
> IBEX,USHI02,ADD,02/10/12,041,02:00:00,02/10/12,041,02:30:00,,LAHO 2K
> Orbit# 155 Payload Recovery
>
>
> Sheral R. Wesley
> SPVR., Satellite Operations
> IBEX Mission OPS
> (304) 279-6678
>
--
Sheral R. Wesley
SPVR., Satellite Operations
IBEX Mission OPS
(304) 279-6678
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; Filename: IBEX_2012_Orbit155_RecoveryContacts_v002.scr
; File type: MAESTRO Absolute Time Sequence Script (ATS)
;
; Create time: 2012/040.142029
; Plan period start: 2012/040.000000
; Plan period stop: 2012/041.235959
; Default time format: UTC
;
; Input files: 3
; IBEX_2012_BLANK_v001.oef
; IBEX_2011_forecast_07feb12-15apr12_v002.sap
; IBEX_2011_9Jan12_Recovery_v001.caf
; ATS_CMD_TIME_OFFSET = 0
script ats_2012_02_09_00_00_00()
begin
@ECT_SetRelay stx,off $TIME=2012/02:09:20:02:00
@ECT_SetRelay stx,on $TIME=2012/02:09:21:28:00
@FMI_SetDownlink2K $TIME=2012/02:09:21:28:02
@FMI_SetBilevelOutputControlReg STXMODE_Strobe,ON $TIME=2012/02:09:21:28:04
@FMI_SetBilevelOutputControlReg COHERENT,ON $TIME=2012/02:09:21:28:06
@ECT_SetRelay stx,off $TIME=2012/02:09:23:02:00
@ECT_SetRelay stx,on $TIME=2012/02:09:23:58:00
@FMI_SetDownlink2K $TIME=2012/02:09:23:58:02
@FMI_SetBilevelOutputControlReg STXMODE_Strobe,ON $TIME=2012/02:09:23:58:04
@FMI_SetBilevelOutputControlReg COHERENT,ON $TIME=2012/02:09:23:58:06
@ECT_SetRelay stx,off $TIME=2012/02:10:01:02:00
@ECT_SetRelay stx,on $TIME=2012/02:10:01:58:00
@FMI_SetDownlink2K $TIME=2012/02:10:01:58:02
@FMI_SetBilevelOutputControlReg STXMODE_Strobe,ON $TIME=2012/02:10:01:58:04
@FMI_SetBilevelOutputControlReg COHERENT,ON $TIME=2012/02:10:01:58:06
@ECT_SetRelay stx,off $TIME=2012/02:10:02:32:00
end
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; Filename: IBEX_2012_Orbit155_RecoverySunMan_v001.scr
; File type: MAESTRO Absolute Time Sequence Script (ATS)
;
; Create time: 2012/039.221622
; Plan period start: 2012/040.000000
; Plan period stop: 2012/041.000000
; Default time format: UTC
;
; Input files: 2
; IBEX_2012_BLANK_v001.oef
; Sun_procession_mnvr_9Feb12_v001.abs
; ATS_CMD_TIME_OFFSET = 0
script ats_2012_02_09_00_00_00()
begin
@FCT_SetScState housekeeping $TIME=2012/02:09:20:54:00
@ECT_SetHTRCmd CATBED_5N_HTR,ON $TIME=2012/02:09:20:55:00
@FCT_SetFcMode burn $TIME=2012/02:09:21:47:00
@ACT_SetLrTarget ACS_SUN $TIME=2012/02:09:21:49:00
@ACT_SetThrustTime 960 $TIME=2012/02:09:21:49:55
@ACT_SetThrustEnable ENABLE $TIME=2012/02:09:21:50:00
@ACT_SetThrustEnable DISABLE $TIME=2012/02:09:22:05:00
@ECT_SetHTRCmd CATBED_5N_HTR,OFF $TIME=2012/02:09:22:05:00
@ACT_SetThrustTime 0 $TIME=2012/02:09:22:05:30
@FCT_SetFcMode Mission $TIME=2012/02:09:22:06:00
end
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