Hi all,
There is a Moderate Eclipse this orbit lasting for 1.1 hours. The long eclipse flag is set for 2 hours before the start and removed ~15 mins after the end, per Ryan Tyler's recommendations.
I have looked at the orbit 0587 ATS file, IBEX_2022_311_o0587a_v001.scr and I approve.
The constraint violations in IBEX_2022_311_o0587a_v001.ccvr are from the removal of the ACT_SetSpinPulseProtectEnable Enable commands and the battery charge dropping because of the eclipse. The violations are acceptable.
The PL commands in IBEX_2022_311_o0587a_v001.scr match those in the STF, IBEX_2022_311_o0587a_v002.stf.
Ascending and descending command sequences are consistent with each other, 15 Re ascending, the apogee maneuver time and 15 Re descending as determined from the OEF, IBEX_2022_311_o0587a_v001.oef and as verified with ibex_orbit.
There is 1 star tracker outages this orbit lasting ~97 hours and ending ~5 hours before the apogee maneuver.
The ground station command sequences are correct and the timing and bit rates match those in the contacts file, IBEX_Orbit587_Contacts.txt for all contacts (3).
The Sun maneuver at perigee of orbit 0586 left us pointing in safe directions for the orbit 0587 arc A ascending and descending sequences:
ibex_rotate -o -r +221.660 -d -16.063 -w ibex-sun -t 2022/11:07:14:48:10
Quaternion +0.000000,+0.000000,+0.000000,+0.000000
points axis +1.000000,+0.000000,+0.000000
towards ECI -0.717934,-0.638757,-0.276694
which is R.A. +221.660 Decl. -16.063
missing R.A. +222.424 Decl. -16.321 (ibex-sun)
error is R.A. +0.764 Decl. +0.258
for a total 0.778 deg
ibex_rotate -o -r +221.660 -d -16.063 -w ibex-sun -t 2022/11:11:23:12:27
Quaternion +0.000000,+0.000000,+0.000000,+0.000000
points axis +1.000000,+0.000000,+0.000000
towards ECI -0.717934,-0.638757,-0.276694
which is R.A. +221.660 Decl. -16.063
missing R.A. +226.737 Decl. -17.505 (ibex-sun)
error is R.A. +5.077 Decl. +1.442
for a total 5.070 deg
The Inertial precession 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 -0.685529,-0.663953,-0.298691 -w ibex-sun -t 2022/11:12:00:55:35
Quaternion +0.000000,+0.000000,+0.000000,+0.000000
points axis +1.000000,+0.000000,+0.000000
towards ECI -0.685529,-0.663953,-0.298691
which is R.A. +224.084 Decl. -17.379
missing R.A. +226.809 Decl. -17.523 (ibex-sun)
error is R.A. +2.725 Decl. +0.144
for a total 2.604 deg
ibex_rotate -o -u -0.685529,-0.663953,-0.298691 -w ibex-sun -t 2022/11:12:02:30:41
Quaternion +0.000000,+0.000000,+0.000000,+0.000000
points axis +1.000000,+0.000000,+0.000000
towards ECI -0.685529,-0.663953,-0.298691
which is R.A. +224.084 Decl. -17.379
missing R.A. +226.875 Decl. -17.540 (ibex-sun)
error is R.A. +2.791 Decl. +0.161
for a total 2.667 deg
ibex_rotate -o -u -0.685529,-0.663953,-0.298691 -w ibex-sun -t 2022/11:16:01:51:25
Quaternion +0.000000,+0.000000,+0.000000,+0.000000
points axis +1.000000,+0.000000,+0.000000
towards ECI -0.685529,-0.663953,-0.298691
which is R.A. +224.084 Decl. -17.379
missing R.A. +230.956 Decl. -18.591 (ibex-sun)
error is R.A. +6.872 Decl. +1.212
for a total 6.647 deg
The Inertial precession maneuver at perigee leaves us pointing in safe directions at the time of the maneuver and at orbit 0588 apogee:
ibex_rotate -o -u -0.624991,-0.712615,-0.318695 -w ibex-sun -t 2022/11:16:04:50:37
Quaternion +0.000000,+0.000000,+0.000000,+0.000000
points axis +1.000000,+0.000000,+0.000000
towards ECI -0.624991,-0.712615,-0.318695
which is R.A. +228.748 Decl. -18.584
missing R.A. +231.092 Decl. -18.629 (ibex-sun)
error is R.A. +2.344 Decl. +0.045
for a total 2.221 deg
ibex_rotate -o -u -0.624991,-0.712615,-0.318695 -w ibex-sun -t 2022-11-21T02:26:32
Quaternion +0.000000,+0.000000,+0.000000,+0.000000
points axis +1.000000,+0.000000,+0.000000
towards ECI -0.624991,-0.712615,-0.318695
which is R.A. +228.748 Decl. -18.584
missing R.A. +236.170 Decl. -19.790 (ibex-sun)
error is R.A. +7.422 Decl. +1.206
for a total 7.112 deg
There is no overlap with orbit 0586 commands.
Command Approval Checklist is attached.
Carol
--
Carol Weaver
University of New Hampshire
503.902.8492
From:
Wesley, Sheral R [US] (SP) <Sheral.Wesley@ngc.com>
Date: Monday, 2022-October-24 at 16:24
To: Ken Fairchild <kwfairchild@gmail.com>
Cc: Perry, Timothy E [US] (SP) <Timothy.Perry@ngc.com>, angoldconsulting <angoldconsulting@earthlink.net>, Carol Weaver <carol.weaver@unh.edu>, Chubin, Eric [US] (SP) <Eric.Chubin@ngc.com>, David Heirtzler <David.Heirtzler@unh.edu>, Kenneth Fairchild
<Ken.Fairchild@unh.edu>, IBEXOPS (IBEXOPS@gmail.com) <ibexops@gmail.com>, ADS-IBEX <ads-ibex@l3harris.com>, ISOC <isocops@lists.sr.unh.edu>, Paul Janzen <Paul.Janzen@mso.umt.edu>, Tyler, Ryan S [US] (SP) <Ryan.Tyler@ngc.com>, Wynn, Reese [US] (SP) <Reese.Wynn@ngc.com>,
Wesley, Sheral R [US] (SP) <Sheral.Wesley@ngc.com>
Subject: IBEX Orbit# 587 ATS Approval (7 Nov 22 - 16 Nov 22)
CAUTION: This email originated from outside of the University System. Do not click links
or open attachments unless you recognize the sender and know the content is safe.
All,
Please review the following for approval.
Approvals are required before
28 Oct 22 @10am
Please note that the PERIGEE Tracking contact on 11/16/22 0600-0700 will end early before the eclipse commands occur.
Please note the following:
-
Moderate Eclipse (PERIGEE)
# 2022-11-16T09:03:01.180Z,EclipseEntry,moderate:true,long:false,orbit:587
# 2022-11-16T10:07:38.814Z,EclipseExit,moderate:true,long:false,orbit:587
2022-11-16T07:00:00 SetLongEclipseFlag TRUE
2022-11-16T10:20:00 SetLongEclipseFlag FALSE
-
Command Load Constraint Violation Report (CCVR)
IBEX_2022_311_o0587a_v001.scr
==========================
HARD CONSTRAINT VIOLATIONS
==========================
NO VIOLATIONS.
==========================
SOFT CONSTRAINT VIOLATIONS
==========================
IBX-CLC-015: Battery charge falls below minimum from 2022/11/16 10:20:00 UTC -
2022/11/16 20:02:00 UTC. Lowest charge level is 392.661308
watt-minutes during this interval.
IBX-CLC-016: No command to enable spin pulse protection was found after
transition to science mode at 2022/11/07 12:31:26 UTC
IBX-CLC-016: No command to enable spin pulse protection was found after
transition to science mode at 2022/11/12 02:00:41 UTC
==============
OTHER MESSAGES
==============
NO MESSAGES.
Sheral Wesley |
Sr Principal Engineer, Satellite Systems
Northrop Grumman Corporation | Space Systems
O: 703-406-5641 | C: 202-236-0802 |
sheral.wesley@ngc.com