[Isocops] IBEX Orbit# 203 ATS (15 Apr 13 - 25 Apr 13) - v001 approve
fair-play at comcast.net
fair-play at comcast.net
Thu Apr 4 14:05:27 EDT 2013
All,
I've looked at the orbit 203 ATS,
IBEX_2013_105_o0203a_v001.scr,
and I approve.
There are no constraint violations in
IBEX_2013_105_o0203a_v001.ccvr.
The PL commands in the v001 ATS match those in the STF,
IBEX_2013_106_o0203a_v001.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 file,
IBEX_2013_105_o0203a_v001.oef,
and as verified with ibex_orbit.
There is a star tracker outage that starts 2- days before perigee and it runs past apogee of orbit 204.
There is one moon in Lo FOV session in arc A. The ATS start time is 8+ hours after that in the OEF and the ATS end time is about 4.5 hours after that in the OEF. These differences are not unusual.
The ground station command sequences are correct and bit rates match those in the contacts file,
IBEX_Orbit203Contacts.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 202 left us pointing in safe directions for orbit 203 arc A ascending and descending sequences:
ibex_rotate -o -u 0.915699,0.37259,0.150571 -w ibex-sun -t 2013/04:16:11:55:45
Quaternion +0.000000,+0.000000,+0.000000,+0.000000
points axis +1.000000,+0.000000,+0.000000
towards ECI +0.915699,+0.372590,+0.150571
which is R.A. +22.141 Decl. +8.660
missing R.A. +24.571 Decl. +10.219 (ibex-sun)
error is R.A. +2.430 Decl. +1.559
for a total 2.859 deg
ibex_rotate -o -u 0.915699,0.37259,0.150571 -w ibex-sun -t 2013/04:20:04:28:38
Quaternion +0.000000,+0.000000,+0.000000,+0.000000
points axis +1.000000,+0.000000,+0.000000
towards ECI +0.915699,+0.372590,+0.150571
which is R.A. +22.141 Decl. +8.660
missing R.A. +28.096 Decl. +11.504 (ibex-sun)
error is R.A. +5.955 Decl. +2.844
for a total 6.516 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 0.880474,0.438854,0.179369 -w ibex-sun -t 2013/04:20:06:11:46
Quaternion +0.000000,+0.000000,+0.000000,+0.000000
points axis +1.000000,+0.000000,+0.000000
towards ECI +0.880474,+0.438854,+0.179369
which is R.A. +26.493 Decl. +10.333
missing R.A. +28.163 Decl. +11.528 (ibex-sun)
error is R.A. +1.670 Decl. +1.195
for a total 2.029 deg
ibex_rotate -o -u 0.880474,0.438854,0.179369 -w ibex-sun -t 2013/04:20:07:46:52
Quaternion +0.000000,+0.000000,+0.000000,+0.000000
points axis +1.000000,+0.000000,+0.000000
towards ECI +0.880474,+0.438854,+0.179369
which is R.A. +26.493 Decl. +10.333
missing R.A. +28.224 Decl. +11.551 (ibex-sun)
error is R.A. +1.731 Decl. +1.218
for a total 2.091 deg
ibex_rotate -o -u 0.880474,0.438854,0.179369 -w ibex-sun -t 2013/04:24:20:38:49
Quaternion +0.000000,+0.000000,+0.000000,+0.000000
points axis +1.000000,+0.000000,+0.000000
towards ECI +0.880474,+0.438854,+0.179369
which is R.A. +26.493 Decl. +10.333
missing R.A. +32.345 Decl. +13.060 (ibex-sun)
error is R.A. +5.852 Decl. +2.727
for a total 6.346 deg
The sun precession maneuver at perigee leaves us pointing in safe directions at the time of the maneuver at at orbit 204 apogee:
ibex_rotate -o -r +32.430 -d +13.091 -w ibex-sun -t 2013/04:24:22:54:05Quaternion +0.000000,+0.000000,+0.000000,+0.000000
points axis +1.000000,+0.000000,+0.000000
towards ECI +0.822112,+0.522332,+0.226498
which is R.A. +32.430 Decl. +13.091
missing R.A. +32.430 Decl. +13.091 (ibex-sun)
error is R.A. +0.000 Decl. +0.000
for a total 0.000 deg
ibex_rotate -o -r +32.430 -d +13.091 -w ibex-sun -t 2013-04-29T21:35:22.173Z
Quaternion +0.000000,+0.000000,+0.000000,+0.000000
points axis +1.000000,+0.000000,+0.000000
towards ECI +0.822112,+0.522332,+0.226498
which is R.A. +32.430 Decl. +13.091
missing R.A. +37.248 Decl. +14.668 (ibex-sun)
error is R.A. +4.818 Decl. +1.577
for a total 4.936 deg
No Lo O-mode.
There is no overlap with orbit 202 commands by manual inspection or by checking at
http://ibex.unh.edu/cgi-bin/ats.cgi .
Command Approval Checklists are attached.
Ken
----- Original Message -----
From: "Ibex Mission Operations" <ibexops at gmail.com>
To: "Bret Hautamaki" <hautamaki.bret at orbital.com>, "IBEX-FDG" <IBEX.fdg at applieddefense.com>, "IBEXOPS/ORB" <IBEXops at orbital.com>, "ISOC at New Hampshire" <isocops at lists.sr.unh.edu>, "John Cavallo" <cavallo.john at orbital.com>, "Mark Tapley" <mtapley at swri.edu>, "Nigel Angold" <ngangold at earthlink.net>, "Robert Lockwood" <Lockwood.Robert at orbital.com>, "Roland Vanderspek" <roland at space.mit.edu>, "Ryan Tyler" <tyler.ryan at orbital.com>, "Sheral Wesley" <wesley.sheral at orbital.com>, "Thomas Regiec" <regiec.thomas at orbital.com>, "Tim Perry" <perry.tim at orbital.com>
Sent: Tuesday, April 2, 2013 1:39:25 PM
Subject: [Isocops] IBEX Orbit# 203 ATS (15 Apr 13 - 25 Apr 13)
Guys,
Here are the planning files and ATS for ORbit# 203.
Please respond to this email thread with all comments/approvals.
All comments/approvals are required before 5 Apr 13 @ 1800 UTC
Note the following:
1. Moon in Lo FOV
# 2013-04-17T14:17:53.366Z,MoonInLoFovStart,orbit:203
# 2013-04-18T17:25:56.084Z,MoonInLoFovStop,orbit:203
2. PERIGEE Sun Maneuver
# 2013-04-23T10:39:53.197Z,StarTrackerOutageStart,orbit:203,dueTo:overlap
# 2013-04-25T18:50:00.000Z,StarTrackerOutageStop,orbit:203,dueTo:overlap
3. Battery Balancing during PERIGEE
4. Command Constraint Violations
# IBEX_2013_105_o0203a_v001.scr
==========================
HARD CONSTRAINT VIOLATIONS
==========================
NO VIOLATIONS.
==========================
SOFT CONSTRAINT VIOLATIONS
==========================
NO VIOLATIONS.
--
Sheral R. Wesley
SPVR., Satellite Operations
IBEX Mission OPS
(304) 279-6678
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