[Isocops] IBEX Orbit# 257 ATS (20 Aug 14 - 29 Aug 14) - v001 approval
Ken Fairchild
fair-play at comcast.net
Sat Aug 9 20:19:55 EDT 2014
All,
I have looked at the orbit 257 ATS,
IBEX_2014_232_o0257a_v001.scr,
and I approve.
There are no constraint violations in
IBEX_2014_232_o0257a_v001.ccvr.
The PL commands in the v001 ATS match those in the v002 STF,
IBEX_2014_232_o0257a_v002.stf.
Ascending and descending command sequences are consistent with each other and 15 Re ascending, the apogee maneuver time and 15 Re descending as determined from the OEF,
IBEX_2014_232_o0257a_v001.oef,
and as verified with ibex_orbit.
There is one star tracker outage. It starts about one hour before perigee and ends about 5 1/2 hours later. No despinning should be required due to this outage.
The are no moon in Lo FOV sessions.
The ground station command sequences are correct and the timing and bit rates match those in the contacts file,
IBEX_Orbit257Contacts.txt,
for all contacts (3).
We are doing battery cell balancing this orbit and the balancing commands are correct and offset by enough time from other commands.
The inertial maneuver at perigee of orbit 256 left us pointing in safe directions for the orbit 257 arc A ascending and descending sequences:
ibex_rotate -o -u -0.814998,0.535516,0.221361 -w ibex-sun -t 2014/08:20:15:49:26
Quaternion +0.000000,+0.000000,+0.000000,+0.000000
points axis +1.000000,+0.000000,+0.000000
towards ECI -0.814998,+0.535516,+0.221361
which is R.A. +146.692 Decl. +12.789
missing R.A. +149.513 Decl. +12.396 (ibex-sun)
error is R.A. +2.821 Decl. +0.393
for a total 2.781 deg
ibex_rotate -o -u -0.814998,0.535516,0.221361 -w ibex-sun -t 2014/08:24:04:33:03
Quaternion +0.000000,+0.000000,+0.000000,+0.000000
points axis +1.000000,+0.000000,+0.000000
towards ECI -0.814998,+0.535516,+0.221361
which is R.A. +146.692 Decl. +12.789
missing R.A. +152.762 Decl. +11.186 (ibex-sun)
error is R.A. +6.070 Decl. +1.603
for a total 6.150 deg
The inertial maneuver at apogee leaves us pointing in safe directions at the time of the maneuver and for arc B ascending and descending sequences:
ibex_rotate -o -u -0.855772,0.478608,0.196442 -w ibex-sun -t 2014/08:24:06:16:11
Quaternion +0.000000,+0.000000,+0.000000,+0.000000
points axis +1.000000,+0.000000,+0.000000
towards ECI -0.855772,+0.478608,+0.196442
which is R.A. +150.783 Decl. +11.329
missing R.A. +152.829 Decl. +11.162 (ibex-sun)
error is R.A. +2.046 Decl. +0.167
for a total 2.014 deg
ibex_rotate -o -u -0.855772,0.478608,0.196442 -w ibex-sun -t 2014/08:24:07:51:17
Quaternion +0.000000,+0.000000,+0.000000,+0.000000
points axis +1.000000,+0.000000,+0.000000
towards ECI -0.855772,+0.478608,+0.196442
which is R.A. +150.783 Decl. +11.329
missing R.A. +152.891 Decl. +11.139 (ibex-sun)
error is R.A. +2.108 Decl. +0.190
for a total 2.076 deg
ibex_rotate -o -u -0.855772,0.478608,0.196442 -w ibex-sun -t 2014/08:28:16:46:04
Quaternion +0.000000,+0.000000,+0.000000,+0.000000
points axis +1.000000,+0.000000,+0.000000
towards ECI -0.855772,+0.478608,+0.196442
which is R.A. +150.783 Decl. +11.329
missing R.A. +156.974 Decl. +9.632 (ibex-sun)
error is R.A. +6.191 Decl. +1.697
for a total 6.319 deg
The inertial maneuver at perigee leaves us pointing in safe directions at the time of the maneuver and at orbit 258 apogee:
ibex_rotate -o -u -0.893226,0.416347,0.169711 -w ibex-sun -t 2014/08:28:18:48:09
Quaternion +0.000000,+0.000000,+0.000000,+0.000000
points axis +1.000000,+0.000000,+0.000000
towards ECI -0.893226,+0.416347,+0.169711
which is R.A. +155.009 Decl. +9.771
missing R.A. +157.050 Decl. +9.604 (ibex-sun)
error is R.A. +2.041 Decl. +0.167
for a total 2.019 deg
ibex_rotate -o -u -0.893226,0.416347,0.169711 -w ibex-sun -t 2014-09-02T15:05:39.648Z
Quaternion +0.000000,+0.000000,+0.000000,+0.000000
points axis +1.000000,+0.000000,+0.000000
towards ECI -0.893226,+0.416347,+0.169711
which is R.A. +155.009 Decl. +9.771
missing R.A. +161.365 Decl. +7.853 (ibex-sun)
error is R.A. +6.356 Decl. +1.918
for a total 6.567 deg
No Lo O-mode.
There is no overlap with orbit 256 commands by manual inspection or by checking at
http://ibex.unh.edu/cgi-bin/ats.cgi .
Command Approval Checklist is attached.
Ken
----- Original Message -----
From: "Ibex Mission Operations" <ibexops at gmail.com>
To: "Harold Kucharek" <Harald.Kucharek at unh.edu>, "IBEX FDG" <ibex at applieddefense.com>, "ISOC at New Hampshire" <isocops at lists.sr.unh.edu>, "Ken Fairchild" <fair-play at comcast.net>, "Marty Quinn" <marty.quinn at unh.edu>, "Michelle Reno" <mreno at swri.edu>, "Nigel Angold" <ngangold at earthlink.net>, "Paul Janzen" <paul.janzen at umontana.edu>, "Robert Lockwood" <Lockwood.Robert at orbital.com>, "Ryan Tyler" <tyler.ryan at orbital.com>, "Sheral Wesley" <wesley.sheral at orbital.com>, "Tim Perry" <perry.tim at orbital.com>
Sent: Thursday, August 7, 2014 11:02:44 AM
Subject: IBEX Orbit# 257 ATS (20 Aug 14 - 29 Aug 14)
Guys,
Here are the planning files and ATS for Orbit# 257.
Please respond to this email thread with comments and approvals.
Approvals are required before 10 Aug 14 @1200 UTC
Please note the following:
1. Battery Balancing at Perigee
ECT_SetLongEclipseFlag TRUE $TIME=2014/08:29:02:00:00
ECT_SetLongEclipseFlag FALSE $TIME=2014/08:29:03:30:00
2. Command Load Constraint Violation Report (CCVR)
IBEX_2014_232_o0257a_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
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