[Isocops] IBEX Orbit# 304 ATS Approval (21 Oct 15 - 30 Oct 15)
Marty Quinn
martyq92 at gmail.com
Fri Oct 9 18:39:34 EDT 2015
Hi All,
I approve the ATS for Orbit 304.
Marty
-------------------------------------------
Orbit 304 Spacecraft Pointing Verifications
-------------------------------------------
ibex_orbit -r 304 -D apogee -R E
ibex_orbit -r 304 -D perigee -R E
ibex_orbit -r 304 -D 14 -R E
ibex_orbit -r 304 -D 15 -R E
#---------------------------------------------------------
#Ibex Orbit position times are in sync with the Command Checklist times.
#---------------------------------------------------------
ibex_orbit -r 304 -D apogee -R E
0304
2015/10:26:05:31:19 1980/01:06:00:00:00
ibex_orbit -r 304 -D perigee -R E
0304
2015/10:30:18:23:25 1980/01:06:00:00:00
ibex_orbit -r 304 -D 14 -R E
0304
2015/10:22:02:15:15 2015/10:30:08:40:19
ibex_orbit -r 304 -D 15 -R E
0304
2015/10:22:03:59:21 2015/10:30:06:56:55
--------------------------------------------------------
#Here are the spacecraft pointing positions for Orbit 304.
#---------------------------------------------------------
#Perigee orbit:303 pointing:
[msq at ena ibexops]$ ibex_rotate -o -u -0.904165,-0.387955,-0.178819 -w
ibex-sun -t 2015/10:21:07:31:06
Quaternion +0.000000,+0.000000,+0.000000,+0.000000
points axis +1.000000,+0.000000,+0.000000
towards ECI -0.904165,-0.387955,-0.178819
which is R.A. +203.223 Decl. -10.301
missing R.A. +205.429 Decl. -10.529 (ibex-sun)
error is R.A. +2.206 Decl. +0.228
for a total 2.181 deg
At beginning of orbit:304 ascending Arc A:
ibex_rotate -o -u -0.904165,-0.387955,-0.178819 -w ibex-sun -t
2015/10:22:03:59:23
Quaternion +0.000000,+0.000000,+0.000000,+0.000000
points axis +1.000000,+0.000000,+0.000000
towards ECI -0.904165,-0.387955,-0.178819
which is R.A. +203.223 Decl. -10.301
missing R.A. +206.219 Decl. -10.851 (ibex-sun)
error is R.A. +2.996 Decl. +0.550
for a total 2.996 deg
At end of orbit:304 descending Arc A:
ibex_rotate -o -u -0.904165,-0.387955,-0.178819 -w ibex-sun -t
2015/10:25:17:55:39
Quaternion +0.000000,+0.000000,+0.000000,+0.000000
points axis +1.000000,+0.000000,+0.000000
towards ECI -0.904165,-0.387955,-0.178819
which is R.A. +203.223 Decl. -10.301
missing R.A. +209.503 Decl. -12.088 (ibex-sun)
error is R.A. +6.280 Decl. +1.787
for a total 6.415 deg
#Apogee orbit:304 pointing:
ibex_rotate -o -u -0.867651,-0.451998,-0.207075 -w ibex-sun -t
2015/10:25:19:38:47
Quaternion +0.000000,+0.000000,+0.000000,+0.000000
points axis +1.000000,+0.000000,+0.000000
towards ECI -0.867651,-0.451998,-0.207075
which is R.A. +207.517 Decl. -11.951
missing R.A. +209.572 Decl. -12.113 (ibex-sun)
error is R.A. +2.055 Decl. +0.162
for a total 2.016 deg
#At beginning of orbit:304 ascending arc B:
ibex_rotate -o -u -0.867651,-0.451998,-0.207075 -w ibex-sun -t
2015/10:25:21:13:53
Quaternion +0.000000,+0.000000,+0.000000,+0.000000
points axis +1.000000,+0.000000,+0.000000
towards ECI -0.867651,-0.451998,-0.207075
which is R.A. +207.517 Decl. -11.951
missing R.A. +209.634 Decl. -12.135 (ibex-sun)
error is R.A. +2.117 Decl. +0.184
for a total 2.079 deg
#At end of orbit:304 descending arc B:
ibex_rotate -o -u -0.867651,-0.451998,-0.207075 -w ibex-sun -t
2015/10:30:06:53:47
Quaternion +0.000000,+0.000000,+0.000000,+0.000000
points axis +1.000000,+0.000000,+0.000000
towards ECI -0.867651,-0.451998,-0.207075
which is R.A. +207.517 Decl. -11.951
missing R.A. +214.001 Decl. -13.612 (ibex-sun)
error is R.A. +6.484 Decl. +1.661
for a total 6.537 deg
#Perigee orbit:304 pointing:
ibex_rotate -o -u -0.825986,-0.513211,-0.233157 -w ibex-sun -t
2015/10:30:09:17:41
Quaternion +0.000000,+0.000000,+0.000000,+0.000000
points axis +1.000000,+0.000000,+0.000000
towards ECI -0.825986,-0.513211,-0.233157
which is R.A. +211.854 Decl. -13.483
missing R.A. +214.103 Decl. -13.647 (ibex-sun)
error is R.A. +2.249 Decl. +0.164
for a total 2.193 deg
#Apogee orbit:304 + 1 pointing:
ibex_rotate -o -u -0.825986,-0.513211,-0.233157 -w ibex-sun -t
2015-11-04T09:25:16
Quaternion +0.000000,+0.000000,+0.000000,+0.000000
points axis +1.000000,+0.000000,+0.000000
towards ECI -0.825986,-0.513211,-0.233157
which is R.A. +211.854 Decl. -13.483
missing R.A. +218.869 Decl. -15.253 (ibex-sun)
error is R.A. +7.015 Decl. +1.770
for a total 7.022 deg
Marty Quinn
GISLAB/Space Science Center UNH
marty.quinn at unh.edu <marty at drsrl.com>
603 988-7107
On Thu, Oct 8, 2015 at 6:12 PM, Wesley.Sheral <sheral.wesley at orbitalatk.com>
wrote:
> Guys,
>
> Here are the planning products and ATS for Orbit# 304. Please respond to
> this email thread with your comments, questions and approvals.
>
> *Approvals are required before 12 Oct 15 @ 1000 UTC*
>
>
>
> Note the following:
>
> 1. Battery balancing at PERIGEE
>
> # Orbit# 304 PERIGEE: Battery Balancing Commands
>
> # 2015-10-30T18:23:26.630Z,Perigee,orbit:304
>
> SetLongEclipseFlag TRUE $TIME=2015/10:30:18:00:00
>
> SetLongEclipseFlag FALSE $TIME=2015/10:30:19:30:00
>
>
>
> 2. IBEX_Hi Gain Test (ascending 30-31 re)
>
> # Orbit# 304 IBEX_Hi Gain Test (23 Oct 15 @ 0600 UTC - 23 Oct 15 @1016
> UTC)
>
>
>
> Sheral R. Wesley
>
> SPVR., Satellite Operations
>
> IBEX Mission OPS
>
> CRS/CYGNUS Mission Planning
>
> Work (703) 406-5641
>
> Cell (304) 279-6678
>
> [image: cid:image001.jpg at 01D04F6C.5A1C97F0]
>
>
>
>
>
>
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