[Isocops] IBEX Orbit# 184 ATS v002 (24 Nov 12 - 2 Nov 12)

[Ibex Mission Operations]

Here is v002 of the *IBEX_2012_298_o0184a_postverif_asc_v002.scr*

The SC commands were commented out
*

*
On Thu, Oct 11, 2012 at 1:51 PM, Ibex Mission Operations
<ibexops at gmail.com>wrote:

> Guys,
>    Here are the planning and ATS files for Orbit# 184.
> Orbit# 184 will also include the LUT Upload.
> The ATS files have not been placed on the SFTP server so that Ken can
> check them individually.
>
>
> 1*.IBEX_2012_298_o0184a_postverif_asc_v001.scr* was generated with
> Ascending payload commands only within the STF
>
> ==========================
> SOFT CONSTRAINT VIOLATIONS
> ==========================
> IBX-CLC-003: Payload mode is HVSCI during interval 2012/10/28 22:24:19 UTC
> -
>              2012/10/28 22:34:19 UTC, which overlaps 5N thruster maneuver
> at
>              2012/10/28 22:24:19 UTC - 2012/10/28 22:34:19 UTC
> IBX-CLC-008: Spacecraft state is HK during interval 2012/10/26 03:45:00
> UTC -
>              2012/10/26 03:59:30 UTC, which overlaps HVSCI payload mode at
>              2012/10/26 03:45:00 UTC - 2012/10/26 03:59:30 UTC
> IBX-CLC-008: Spacecraft state is HK during interval 2012/10/26 03:59:30
> UTC -
>              2012/10/29 18:25:00 UTC, which overlaps HVSCI payload mode at
>              2012/10/26 03:59:30 UTC - 2012/10/29 18:25:00 UTC
>
>
>
> --
> Sheral R. Wesley
> SPVR., Satellite Operations
> IBEX Mission OPS
> (304) 279-6678
>



-- 
Sheral R. Wesley
SPVR., Satellite Operations
IBEX Mission OPS
(304) 279-6678
-------------- next part --------------
An HTML attachment was scrubbed...
URL: http://lists.sr.unh.edu/mailman/private/isocops/attachments/20121016/c8998805/attachment-0001.html 
-------------- next part --------------
; Filename:            IBEX_2012_298_o0184a_postverif_asc_v002.scr
; File type:           MAESTRO Absolute Time Sequence Script (ATS)
;
; Create time:         2012/285.163319
; Plan period start:   2012/299.031900
; Plan period stop:    2012/303.182500
; Default time format: UTC
;
; Input files:         2
;   IBEX_2012_298_o0184a_v001.oef
;   IBEX_2012_298_o0184a_postverif_asc_v001.stf
; ATS_CMD_TIME_OFFSET = 0
script ats_2012_10_25_03_19_00()
begin
#  Orbit# 184 Ascending Payload Commands
  @CEU_MACRO_EXEC ASCENDING_PL1 $TIME=2012/10:26:03:45:00
  @CEU_MACRO_EXEC ASCENDING_HI $TIME=2012/10:26:03:45:30
  @CEU_MACRO_EXEC ASCENDING_PL2 $TIME=2012/10:26:03:57:00
  @CEU_MACRO_EXEC ASCENDING_PL1 $TIME=2012/10:26:03:59:30
  @CEU_MACRO_EXEC ASCENDING_LO $TIME=2012/10:26:04:00:00
  @CEU_MACRO_EXEC ASCENDING_PL2 $TIME=2012/10:26:04:08:30
  
#  Orbit# 184 APOGEE: Inertial MAneuver  
#  @ECT_SetHTRCmd CATBED_5N_HTR,ON $TIME=2012/10:28:21:29:19
#  @ACT_SetKFInputSelect GND_CMD, 0, 0, 0, 0 $TIME=2012/10:28:22:14:19
#  @ACT_SetEstUpdateEnables ENABLE, DISABLE $TIME=2012/10:28:22:14:20
#  @FCT_SetFcMode burn $TIME=2012/10:28:22:21:19
#  @ACT_SetInrDir -0.832247,-0.50355,-0.231952 $TIME=2012/10:28:22:22:19
#  @ACT_SetLrTarget ACS_INERTIAL $TIME=2012/10:28:22:23:19
#  @ACT_SetThrustTime 660 $TIME=2012/10:28:22:24:14
#  @ACT_SetThrustEnable ENABLE $TIME=2012/10:28:22:24:19
#  @ACT_SetThrustEnable DISABLE $TIME=2012/10:28:22:34:19
#  @ECT_SetHTRCmd CATBED_5N_HTR,OFF $TIME=2012/10:28:22:34:20
#  @ACT_SetThrustTime 0 $TIME=2012/10:28:22:34:49
#  @ACT_SetStaticZrate ESTIMATOR, 0.418 $TIME=2012/10:28:22:49:29
#  @ACT_SetKFInputSelect STA_PCT_VALID, 48,18,23,53 $TIME=2012/10:28:22:49:39
#  @FCT_SetFcMode Mission $TIME=2012/10:28:22:50:19
end