[Isocops] IBEX Orbit #602 ATS Approval (22 - 31 Mar 2023)

Carol Weaver Carol.Weaver at unh.edu
Mon Mar 13 09:47:04 EDT 2023


Hi all,
I have looked at the orbit 0602 ATS file, IBEX_2023_081_o0602a_v001.scr and I approve.

The constraint violations in IBEX_2023_081_o0602a_v001.ccvr are from the removal of the ACT_SetSpinPulseProtectEnable Enable commands. The violations are acceptable.

The PL commands in IBEX_2023_081_o0602a_v001.scr match those in the STF, IBEX_2023_081_o0602a_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_2023_081_o0602a_v001.oef and as verified with ibex_orbit.

There is 1 star tracker outage this orbit lasting for ~7.5 hours and ending ~1.2 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_Orbit602_Contacts.txt for all contacts (3).

Battery Balancing is 90 minutes long, more than 2 hours away from payload descending macros, and more than 15 minutes away from a maneuver.

The Inertial maneuver at perigee of orbit 0601 left us pointing in safe directions for the orbit 0602 arc A ascending and descending sequences:

ibex_rotate -o -u 0.999941,0.009023,-0.006126  -w ibex-sun -t 2023/03:22:13:28:02
Quaternion    +0.000000,+0.000000,+0.000000,+0.000000
points axis  +1.000000,+0.000000,+0.000000
towards ECI  +0.999941,+0.009023,-0.006126
which is     R.A.   +0.517 Decl.  -0.351
missing      R.A.   +1.213 Decl.  +0.505 (ibex-sun)
error is     R.A.   +0.696 Decl.  +0.856
for a total  1.103 deg

ibex_rotate -o -u 0.999941,0.009023,-0.006126  -w ibex-sun -t 2023/03:26:06:46:51
Quaternion    +0.000000,+0.000000,+0.000000,+0.000000
points axis  +1.000000,+0.000000,+0.000000
towards ECI  +0.999941,+0.009023,-0.006126
which is     R.A.   +0.517 Decl.  -0.351
missing      R.A.   +4.701 Decl.  +2.042 (ibex-sun)
error is     R.A.   +4.184 Decl.  +2.393
for a total  4.819 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 0.998419,0.054719,0.01288 -w ibex-sun -t 2023/03:26:08:29:59
Quaternion    +0.000000,+0.000000,+0.000000,+0.000000
points axis  +1.000000,+0.000000,+0.000000
towards ECI  +0.998419,+0.054719,+0.012880
which is     R.A.   +3.137 Decl.  +0.738
missing      R.A.   +4.767 Decl.  +2.071 (ibex-sun)
error is     R.A.   +1.630 Decl.  +1.333
for a total  2.105 deg

ibex_rotate -o -u 0.998419,0.054719,0.01288 -w ibex-sun -t 2023/03:26:10:05:05
Quaternion    +0.000000,+0.000000,+0.000000,+0.000000
points axis  +1.000000,+0.000000,+0.000000
towards ECI  +0.998419,+0.054719,+0.012880
which is     R.A.   +3.137 Decl.  +0.738
missing      R.A.   +4.827 Decl.  +2.098 (ibex-sun)
error is     R.A.   +1.690 Decl.  +1.360
for a total  2.169 deg

ibex_rotate -o -u 0.998419,0.054719,0.01288 -w ibex-sun -t 2023/03:30:22:12:51
Quaternion    +0.000000,+0.000000,+0.000000,+0.000000
points axis  +1.000000,+0.000000,+0.000000
towards ECI  +0.998419,+0.054719,+0.012880
which is     R.A.   +3.137 Decl.  +0.738
missing      R.A.   +8.840 Decl.  +3.827 (ibex-sun)
error is     R.A.   +5.703 Decl.  +3.089
for a total  6.482 deg

The Inertial precession maneuver at perigee leaves us pointing in safe directions at the time of the maneuver and at orbit 0603 apogee:

ibex_rotate -o -u 0.990755,0.12778,0.045572 -w ibex-sun -t 2023/03:31:03:09:26
Quaternion    +0.000000,+0.000000,+0.000000,+0.000000
points axis  +1.000000,+0.000000,+0.000000
towards ECI  +0.990755,+0.127780,+0.045572
which is     R.A.   +7.349 Decl.  +2.612
missing      R.A.   +9.019 Decl.  +3.894 (ibex-sun)
error is     R.A.   +1.670 Decl.  +1.282
for a total  2.103 deg

ibex_rotate -o -u 0.990755,0.12778,0.045572 -w ibex-sun -t 2023-04-04T21:57:43
Quaternion    +0.000000,+0.000000,+0.000000,+0.000000
points axis  +1.000000,+0.000000,+0.000000
towards ECI  +0.990755,+0.127780,+0.045572
which is     R.A.   +7.349 Decl.  +2.612
missing      R.A.  +13.468 Decl.  +5.779 (ibex-sun)
error is     R.A.   +6.119 Decl.  +3.167
for a total  6.875 deg

There is no overlap with orbit 0601 commands.

Command Approval Checklist is attached.

Carol

--
Carol Weaver
University of New Hampshire
503-902-8492

From: NIgel Angold <nangold at princeton.edu>
Date: Sunday, March 12, 2023 at 18:15
To: Perry, Timothy E [US] (SP) <Timothy.Perry at ngc.com>
Cc: Carol Weaver <carol.weaver at unh.edu>, Chubin, Eric [US] (SP) <Eric.Chubin at ngc.com>, David Heirtzler <David.Heirtzler at unh.edu>, IBEX FDG Group <ADS-IBEX at l3harris.com>, IBEXOPS <ibexops at gmail.com>, ISOC <isocops at lists.sr.unh.edu>, Ken Fairchild <fair-play at comcast.net>, Ken Fairchild (kwfairchild at gmail.com) <kwfairchild at gmail.com>, Kenneth Fairchild <Ken.Fairchild at unh.edu>, angoldconsulting <angoldconsulting at earthlink.net>, Paul Janzen <paul.janzen at mso.umt.edu>, Tyler, Ryan S [US] (SP) <Ryan.Tyler at ngc.com>, Wesley, Sheral R [US] (SP) <Sheral.Wesley at ngc.com>, Wynn, Reese [US] (SP) <Reese.Wynn at ngc.com>
Subject: Re: [Isocops] IBEX Orbit #602 ATS Approval (22 - 31 Mar 2023)
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.

I approve IBEX_2023_081_o0602a_v001.scr

Nigel

Perry, Timothy E [US] (SP)<mailto:Timothy.Perry at ngc.com>
March 9, 2023 at 08:04
All,
   Attached are the planning files for Orbit #602. Please respond to this thread with comments and approvals.
Approvals are required by COB, 12 Mar 2023

Please note the following:

1.       Battery Balancing this orbit

Begin 2023/03/31 08:00:00– End 2023/03/31 09:30:00


2.       Command Load Constraint Violation Report (CCVR)
IBEX_2023_081_o0602a_v001.ccvr
# Input files:         1
#   IBEX_2023_081_o0602a_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 2023/03/22 11:09:13 UTC
IBX-CLC-016: No command to enable spin pulse protection was found after
             transition to science mode at 2023/03/26 09:35:05 UTC

==============
OTHER MESSAGES
==============
NO MESSAGES.





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