Hi all,
I have looked at the orbit 0562 ATS file, IBEX_2022_083_o0562a_v001.scr and I approve.
The constraint violations in IBEX_2022_083_o0562a_v001.ccvr are from the removal of the ACT_SetSpinPulseProtectEnable Enable commands. The violations are acceptable.
The PL commands in IBEX_2022_083_o0562a_v001.scr match those in the STF, IBEX_2022_083_o0562a_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_083_o0562a_v001.oef and as verified with ibex_orbit.
There is 1 star tracker outage this orbit lasting ~4.5 hours and ending ~5.3 hours before the perigee maneuver.
The ground station command sequences are correct and the timing and bit rates match those in the contacts file, IBEX_Orbit562_Contacts.txt for all contacts (2).
No Battery Balancing this orbit.
The Inertial maneuver at perigee of orbit 0561 left us pointing in safe directions for the orbit 0562 arc A ascending and descending sequences:
ibex_rotate -o -u 0.999527,0.030573,0.003438 -w ibex-sun -t 2022/03:25:07:53:53
Quaternion +0.000000,+0.000000,+0.000000,+0.000000
points axis +1.000000,+0.000000,+0.000000
towards ECI +0.999527,+0.030573,+0.003438
which is R.A. +1.752 Decl. +0.197
missing R.A. +3.965 Decl. +1.697 (ibex-sun)
error is R.A. +2.213 Decl. +1.500
for a total 2.673 deg
ibex_rotate -o -u 0.999527,0.030573,0.003438 -w ibex-sun -t 2022/03:29:00:29:17
Quaternion +0.000000,+0.000000,+0.000000,+0.000000
points axis +1.000000,+0.000000,+0.000000
towards ECI +0.999527,+0.030573,+0.003438
which is R.A. +1.752 Decl. +0.197
missing R.A. +7.431 Decl. +3.212 (ibex-sun)
error is R.A. +5.679 Decl. +3.015
for a total 6.427 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 0.99421,0.102145,0.033365 -w ibex-sun -t 2022/03:29:02:12:25
Quaternion +0.000000,+0.000000,+0.000000,+0.000000
points axis +1.000000,+0.000000,+0.000000
towards ECI +0.994210,+0.102145,+0.033365
which is R.A. +5.866 Decl. +1.912
missing R.A. +7.496 Decl. +3.242 (ibex-sun)
error is R.A. +1.630 Decl. +1.330
for a total 2.103 deg
ibex_rotate -o -u 0.99421,0.102145,0.033365 -w ibex-sun -t 2022/03:29:03:47:31
Quaternion +0.000000,+0.000000,+0.000000,+0.000000
points axis +1.000000,+0.000000,+0.000000
towards ECI +0.994210,+0.102145,+0.033365
which is R.A. +5.866 Decl. +1.912
missing R.A. +7.557 Decl. +3.269 (ibex-sun)
error is R.A. +1.691 Decl. +1.357
for a total 2.166 deg
ibex_rotate -o -u 0.99421,0.102145,0.033365 -w ibex-sun -t 2022/04:02:14:59:25
Quaternion +0.000000,+0.000000,+0.000000,+0.000000
points axis +1.000000,+0.000000,+0.000000
towards ECI +0.994210,+0.102145,+0.033365
which is R.A. +5.866 Decl. +1.912
missing R.A. +11.526 Decl. +4.964 (ibex-sun)
error is R.A. +5.660 Decl. +3.052
for a total 6.421 deg
The Inertial precession maneuver at perigee leaves us pointing in safe directions at the time of the maneuver and at orbit 0563 apogee:
ibex_rotate -o -u 0.982755,0.173039,0.065194 -w ibex-sun -t 2022/04:02:18:45:04
Quaternion +0.000000,+0.000000,+0.000000,+0.000000
points axis +1.000000,+0.000000,+0.000000
towards ECI +0.982755,+0.173039,+0.065194
which is R.A. +9.986 Decl. +3.738
missing R.A. +11.663 Decl. +5.015 (ibex-sun)
error is R.A. +1.677 Decl. +1.277
for a total 2.104 deg
ibex_rotate -o -u 0.982755,0.173039,0.065194 -w ibex-sun -t 2022-04-07T14:44:28
Quaternion +0.000000,+0.000000,+0.000000,+0.000000
points axis +1.000000,+0.000000,+0.000000
towards ECI +0.982755,+0.173039,+0.065194
which is R.A. +9.986 Decl. +3.738
missing R.A. +16.181 Decl. +6.900 (ibex-sun)
error is R.A. +6.195 Decl. +3.162
for a total 6.931 deg
There is no overlap with orbit 0561 commands.
Command Approval Checklist is attached.
Carol
--
Carol Weaver
University of New Hampshire
503.902.8492
From:
Perry, Timothy E [US] (SP) <Timothy.Perry@ngc.com>
Date: Friday, 2022-March-11 at 10:54
To: Carol Weaver <carol.weaver@unh.edu>, Chubin, Eric [US] (SP) <Eric.Chubin@ngc.com>, David Heirtzler <David.Heirtzler@unh.edu>, ADS-IBEX@l3harris.com <ADS-IBEX@l3harris.com>, IBEXOPS@gmail.com <IBEXOPS@gmail.com>, isocops@lists.sr.unh.edu <isocops@lists.sr.unh.edu>,
fair-play@comcast.net <fair-play@comcast.net>, kwfairchild@gmail.com <kwfairchild@gmail.com>, Kenneth Fairchild <Ken.Fairchild@unh.edu>, angoldconsulting@earthlink.net <angoldconsulting@earthlink.net>, Paul.Janzen@mso.umt.edu <Paul.Janzen@mso.umt.edu>, Perry,
Timothy E [US] (SP) <Timothy.Perry@ngc.com>, Tyler, Ryan S [US] (SP) <Ryan.Tyler@ngc.com>, Wesley, Sheral R [US] (SP) <Sheral.Wesley@ngc.com>, Wynn, Reese [US] (SP) <Reese.Wynn@ngc.com>
Subject: IBEX Orbit #562 ATS Approval (24 Mar – 03 Apr 2022)
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All,
Attached are the planning files for Orbit #562. Please respond to this thread with comments and approvals.
Approvals are required by COB, 14 Mar 2022
Please note the following:
IBEX_2022_083_o0562a_v001.ccvr
# Input files: 1
# IBEX_2022_083_o0562a_v001.scr
==========================
HARD CONSTRAINT VIOLATIONS
==========================
NO VIOLATIONS.
==========================
SOFT CONSTRAINT VIOLATIONS
==========================
IBX-CLC-016: No command to enable spin pulse protection was found after
transition to science mode at 2022/03/25 04:36:31 UTC
IBX-CLC-016: No command to enable spin pulse protection was found after
transition to science mode at 2022/03/29 03:17:31 UTC
==============
OTHER MESSAGES
==============
NO MESSAGES.
Timothy E.Perry
CRS IBEX OCO-2
Mission Operations
timothy.perry@ngc.com
Office (703) 406-5976
Cell (301) 606-1430