[Isocops] IBEX Orbit# 291 ATS (24 Jun 15 - 3 Jul 15)

Marty Quinn martyq92 at gmail.com
Thu Jun 11 14:00:01 EDT 2015


Hi All,

I approve orbit 291 ATS commands.

NOTE: the transition to housekeeping occurs  651.5 minutes before thrust
enable presumably due to the insertion of the contact prior to maneuver.

There are two moon in FOV sessions, the second one presumably ends during
apogee.

The orbit pointing follows.

Regards,

Marty

-------------------------------------------
Orbit 291 Spacecraft Pointing Verifications
-------------------------------------------

ibex_orbit -r 291 -D apogee -R E
ibex_orbit -r 291 -D perigee -R E
ibex_orbit -r 291 -D 14 -R E
ibex_orbit -r 291 -D 15 -R E
#---------------------------------------------------------
#Ibex Orbit positions times are in sync with the Command Checklist times.
#---------------------------------------------------------
[msq at ena ~]$ ibex_orbit -r 291 -D apogee -R E
0291
2015/06:28:23:04:37
[msq at ena ~]$ ibex_orbit -r 291 -D perigee -R E
0291
2015/07:03:10:47:14
[msq at ena ~]$ ibex_orbit -r 291 -D 14 -R E
0291
2015/06:24:21:19:54 2015/07:03:00:18:34
[msq at ena ~]$ ibex_orbit -r 291 -D 15 -R E
0291
2015/06:24:22:47:15 2015/07:02:22:53:02



#---------------------------------------------------------
#Here are the spacecraft pointing positions for Orbit 291.
#---------------------------------------------------------
[msq at ena 290]$ #Perigee Orbit 290 pointing:
[msq at ena 290]$ ibex_rotate -o -u -0.003892,0.921354,0.388706   -w ibex-sun
-t 2015/06:24:01:09:42
Quaternion    +0.000000,+0.000000,+0.000000,+0.000000
 points axis  +1.000000,+0.000000,+0.000000
 towards ECI  -0.003892,+0.921354,+0.388706
 which is     R.A.  +90.242 Decl. +22.874
 missing      R.A.  +92.245 Decl. +23.433 (ibex-sun)
 error is     R.A.   +2.003 Decl.  +0.559
 for a total  1.925 deg

#At beginning of orbit:291 ascending Arc A:
ibex_rotate -o -u -0.003892,0.921354,0.388706   -w ibex-sun -t
2015/06:24:22:47:17
Quaternion    +0.000000,+0.000000,+0.000000,+0.000000
 points axis  +1.000000,+0.000000,+0.000000
 towards ECI  -0.003892,+0.921354,+0.388706
 which is     R.A.  +90.242 Decl. +22.874
 missing      R.A.  +93.118 Decl. +23.397 (ibex-sun)
 error is     R.A.   +2.876 Decl.  +0.523
 for a total  2.696 deg

#at end of orbit:291 descending Arc A:
ibex_rotate -o -u -0.003892,0.921354,0.388706  -w ibex-sun -t
2015/06:28:11:32:10
Quaternion    +0.000000,+0.000000,+0.000000,+0.000000
 points axis  +1.000000,+0.000000,+0.000000
 towards ECI  -0.003892,+0.921354,+0.388706
 which is     R.A.  +90.242 Decl. +22.874
 missing      R.A.  +96.867 Decl. +23.253 (ibex-sun)
 error is     R.A.   +6.625 Decl.  +0.379
 for a total  6.107 deg

#Apogee orbit:291 pointing:
Quaternion    +0.000000,+0.000000,+0.000000,+0.000000
 points axis  +1.000000,+0.000000,+0.000000
 towards ECI  -0.077295,+0.918753,+0.387194
 which is     R.A.  +94.809 Decl. +22.780
 missing      R.A.  +96.943 Decl. +23.250 (ibex-sun)
 error is     R.A.   +2.134 Decl.  +0.470
 for a total  2.020 deg

 #At beginning of  orbit:291 ascending arc B:
Quaternion    +0.000000,+0.000000,+0.000000,+0.000000
 points axis  +1.000000,+0.000000,+0.000000
 towards ECI  -0.077295,+0.918753,+0.387194
 which is     R.A.  +94.809 Decl. +22.780
 missing      R.A.  +97.013 Decl. +23.247 (ibex-sun)
 error is     R.A.   +2.204 Decl.  +0.467
 for a total  2.082 deg

#At end of  orbit:291 descending arc B:
Quaternion    +0.000000,+0.000000,+0.000000,+0.000000
 points axis  +1.000000,+0.000000,+0.000000
 towards ECI  -0.077295,+0.918753,+0.387194
 which is     R.A.  +94.809 Decl. +22.780
 missing      R.A. +101.484 Decl. +23.029 (ibex-sun)
 error is     R.A.   +6.675 Decl.  +0.249
 for a total  6.153 deg

#Perigee orbit:291 pointing:
Quaternion    +0.000000,+0.000000,+0.000000,+0.000000
 points axis  +1.000000,+0.000000,+0.000000
 towards ECI  -0.152836,+0.910580,+0.384037
 which is     R.A.  +99.528 Decl. +22.584
 missing      R.A. +101.953 Decl. +22.990 (ibex-sun)
 error is     R.A.   +2.425 Decl.  +0.406
 for a total  2.272 deg

#Apogee orbit:291 + 1 pointing:
Quaternion    +0.000000,+0.000000,+0.000000,+0.000000
 points axis  +1.000000,+0.000000,+0.000000
 towards ECI  -0.152836,+0.910580,+0.384037
 which is     R.A.  +99.528 Decl. +22.584
 missing      R.A. +106.638 Decl. +22.524 (ibex-sun)
 error is     R.A.   +7.110 Decl.  +0.060
 for a total  6.566 deg






Marty Quinn
GISLAB/Space Science Center UNH
marty.quinn at unh.edu <marty at drsrl.com>
603 988-7107

On Thu, Jun 11, 2015 at 11:51 AM, Ibex Mission Operations <ibexops at gmail.com
> wrote:

> Guys,
> Here are the planning files and ATS for Orbit# 291. Please respond to this
> email thread with questions, comments and approvals.
> Approvals are required before 14 June 15 @ 1400 UTC
> ​Note the following;
> 1. Perigee Battery Balancing​
> # Orbit# 291 PERIGEE: Battery Balancing Commands
> # 2015-07-03T10:47:14.720Z,Perigee,orbit:291
>   @ECT_SetLongEclipseFlag TRUE $TIME=2015/07:03:12:00:00
>   @ECT_SetLongEclipseFlag FALSE $TIME=2015/07:03:13:30:00
> # 2015-07-03T14:37:25.782Z,10RECrossing,oMode:0,direction:asc,orbit:291
>
> ​2. Moon in Lo FOV
>
> # 2015-06-25T00:13:42.673Z,MoonInLoFovStart,orbit:291
> # 2015-06-28T10:29:38.805Z,MoonInLoFovStop,orbit:291
>
> 3. Command Load Constraint Violation Report
> IBEX_2015_175_o0291a_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
>
>
>
> Please restrict discussions on this email list to non-ITAR sensitive
> topics.
> ______________________________________________
> Isocops mailing list
> Isocops at lists.sr.unh.edu
> http://lists.sr.unh.edu/mailman/listinfo/isocops
>
>
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