[Isocops] IBEX Orbit# 300 ATS Approval
Marty Quinn
martyq92 at gmail.com
Wed Sep 2 18:30:41 EDT 2015
Hi All,
I approve the ATS for Orbit 300.
The pointing details are below.
Regards,
Marty
-------------------------------------------
Orbit 300 Spacecraft Pointing Verifications
-------------------------------------------
ibex_orbit -r 300 -D apogee -R E
ibex_orbit -r 300 -D perigee -R E
ibex_orbit -r 300 -D 14 -R E
ibex_orbit -r 300 -D 15 -R E
#---------------------------------------------------------
#Ibex Orbit positions times are in sync with the Command Checklist times.
#---------------------------------------------------------
ibex_orbit -r 300 -D apogee -R E
0300
2015/09:19:11:40:50
[msq at ena 300]$ ibex_orbit -r 300 -D perigee -R E
0300
2015/09:24:01:58:41
[msq at ena 300]$ ibex_orbit -r 300 -D 14 -R E
0300
2015/09:15:07:37:27 2015/09:23:16:08:12
[msq at ena 300]$ ibex_orbit -r 300 -D 15 -R E
0300
2015/09:15:09:17:16 2015/09:23:14:27:43
14 15 re ascending
2015/09:15:07:37:27 2015/09:15:09:17:16
15 14 re descending
2015/09:23:14:27:43 2015/09:23:16:08:12
#---------------------------------------------------------
#Here are the spacecraft pointing positions for Orbit 300.
#---------------------------------------------------------
#Perigee orbit:299 pointing:
ibex_rotate -o -u -0.982198,0.176,0.065664 -w ibex-sun -t
2015/09:14:12:34:00
Quaternion +0.000000,+0.000000,+0.000000,+0.000000
points axis +1.000000,+0.000000,+0.000000
towards ECI -0.982198,+0.176000,+0.065664
which is R.A. +169.841 Decl. +3.765
missing R.A. +171.923 Decl. +3.501 (ibex-sun)
error is R.A. +2.082 Decl. +0.264
for a total 2.094 deg
At beginning of orbit:300 ascending Arc A:
ibex_rotate -o -u -0.982198,0.176,0.065664 -w ibex-sun -t
2015/09:15:09:17:18
Quaternion +0.000000,+0.000000,+0.000000,+0.000000
points axis +1.000000,+0.000000,+0.000000
towards ECI -0.982198,+0.176000,+0.065664
which is R.A. +169.841 Decl. +3.765
missing R.A. +172.645 Decl. +3.167 (ibex-sun)
error is R.A. +2.804 Decl. +0.598
for a total 2.862 deg
At end of orbit:300 descending Arc A:
ibex_rotate -o -u -0.982198,0.176,0.065664 -w ibex-sun -t
2015/09:19:00:07:01
Quaternion +0.000000,+0.000000,+0.000000,+0.000000
points axis +1.000000,+0.000000,+0.000000
towards ECI -0.982198,+0.176000,+0.065664
which is R.A. +169.841 Decl. +3.765
missing R.A. +175.815 Decl. +1.776 (ibex-sun)
error is R.A. +5.974 Decl. +1.989
for a total 6.290 deg
#Apogee orbit:300 pointing:
ibex_rotate -o -u -0.9937,0.106459,0.035022 -w ibex-sun -t
2015/09:19:01:50:09
Quaternion +0.000000,+0.000000,+0.000000,+0.000000
points axis +1.000000,+0.000000,+0.000000
towards ECI -0.993700,+0.106459,+0.035022
which is R.A. +173.885 Decl. +2.007
missing R.A. +175.880 Decl. +1.748 (ibex-sun)
error is R.A. +1.995 Decl. +0.259
for a total 2.011 deg
#At beginning of orbit:300 ascending arc B:
ibex_rotate -o -u -0.9937,0.106459,0.035022 -w ibex-sun -t
2015/09:19:03:25:15
Quaternion +0.000000,+0.000000,+0.000000,+0.000000
points axis +1.000000,+0.000000,+0.000000
towards ECI -0.993700,+0.106459,+0.035022
which is R.A. +173.885 Decl. +2.007
missing R.A. +175.940 Decl. +1.723 (ibex-sun)
error is R.A. +2.055 Decl. +0.285
for a total 2.074 deg
#At end of orbit:300 descending arc B:
ibex_rotate -o -u -0.9937,0.106459,0.035022 -w ibex-sun -t
2015/09:23:14:24:35
Quaternion +0.000000,+0.000000,+0.000000,+0.000000
points axis +1.000000,+0.000000,+0.000000
towards ECI -0.993700,+0.106459,+0.035022
which is R.A. +173.885 Decl. +2.007
missing R.A. +180.061 Decl. -0.010 (ibex-sun)
error is R.A. +6.176 Decl. +2.017
for a total 6.496 deg
#Perigee orbit:300 pointing:
ibex_rotate -o -u -0.999414,0.033975,0.004119 -w ibex-sun -t
2015/09:23:16:47:26
Quaternion +0.000000,+0.000000,+0.000000,+0.000000
points axis +1.000000,+0.000000,+0.000000
towards ECI -0.999414,+0.033975,+0.004119
which is R.A. +178.053 Decl. +0.236
missing R.A. +180.151 Decl. -0.050 (ibex-sun)
error is R.A. +2.098 Decl. +0.286
for a total 2.117 deg
#Apogee orbit:300 + 1 pointing:
ibex_rotate -o -u -0.999414,0.033975,0.004119 -w ibex-sun -t
2015-09-28T15:19:25
Quaternion +0.000000,+0.000000,+0.000000,+0.000000
points axis +1.000000,+0.000000,+0.000000
towards ECI -0.999414,+0.033975,+0.004119
which is R.A. +178.053 Decl. +0.236
missing R.A. +184.464 Decl. -1.966 (ibex-sun)
error is R.A. +6.411 Decl. +2.202
for a total 6.777 deg
Marty Quinn
GISLAB/Space Science Center UNH
marty.quinn at unh.edu <marty at drsrl.com>
603 988-7107
On Tue, Sep 1, 2015 at 11:14 AM, Wesley.Sheral <sheral.wesley at orbitalatk.com
> wrote:
> Guys,
>
> We have finally
>
> Here are the planning products and ATS for Orbit# 300. Please respond
> to this email thread with your comments, questions and approvals.
>
> Approvals are required before 4 Sept 14 @ 1300 UTC
>
>
>
> Note the following
>
> 1. Battery Balancing at PERIGEE
>
> Orbit# 300 PERIGEE: Battery Balancing Commands
>
> # 2015-09-24T01:58:42.514Z,Perigee,orbit:300
>
> SetLongEclipseFlag TRUE $TIME=2015/09:24:01:00:00
>
> SetLongEclipseFlag FALSE $TIME=2015/09:24:02:30:00
>
>
>
> 2. Moon in Lo FOV
>
> Orbit# 300 APOGEE: Moon in Lo FOV Commands
>
> # 2015-09-22T15:23:21.648Z,MoonInLoFovStart,orbit:300
>
> # 2015-09-23T04:48:37.267Z,MoonInLoFovStop,orbit:300
>
>
>
> 3. Command Load Constraint Violation Report
>
> IBEX_2015_257_o0300a_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
>
> CRS/CYGNUS Mission Planning
>
> Work (703) 406-5641
>
> Cell (304) 279-6678
>
> [image: cid:image001.jpg at 01D04F6C.5A1C97F0]
>
>
>
>
>
>
> ------------------------------------------------------------------------------
>
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