Hi all,

I have looked at the orbit 0671 ATS file, IBEX_2024_345_o0671a_v001.scr and I approve.

 

The constraint violations in IBEX_2024_345_o0671a_v001.ccvr are from the removal of the ACT_SetSpinPulseProtectEnable Enable commands and transmissions being close together. The violations are acceptable.

 

The PL commands in IBEX_2024_345_o0671a_v001.scr match those in the STF, IBEX_2024_345_o0671a_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_2024_345_o0671a_v001.oef and as verified with ibex_orbit.

 

There is 1 star tracker outage this orbit. Outage begins at 2024-12-14 15:38:01 and lasts for 86.1 hours. 

  

The ground station command sequences are correct and the timing and bit rates match those in the contacts file, IBEX_Orbit671_Contacts.txt for all contacts (3).

 

Battery Balancing is 90 minutes long, more than 2 hours away from payload descending macros, 11.733 hrs, and more than 15 minutes away from a maneuver, 586 mins.

 

 

 

The Inertial maneuver at perigee of orbit 0670 left us pointing in safe directions for the orbit 0671 arc A ascending and descending sequences:

 

ibex_rotate -o -u -0.176393,-0.899168,-0.400477  -w ibex-sun -t 2024/12:11:01:47:21

Quaternion    +0.000000,+0.000000,+0.000000,+0.000000

points axis  +1.000000,+0.000000,+0.000000

towards ECI  -0.176393,-0.899168,-0.400477

which is     R.A. +258.901 Decl. -23.608

missing      R.A. +258.256 Decl. -23.012 (ibex-sun)

error is     R.A.   +0.645 Decl.  +0.596

for a total  0.840 deg

 

ibex_rotate -o -u -0.176393,-0.899168,-0.400477  -w ibex-sun -t 2024/12:14:02:18:17

Quaternion    +0.000000,+0.000000,+0.000000,+0.000000

points axis  +1.000000,+0.000000,+0.000000

towards ECI  -0.176393,-0.899168,-0.400477

which is     R.A. +258.901 Decl. -23.608

missing      R.A. +261.618 Decl. -23.195 (ibex-sun)

error is     R.A.   +2.717 Decl.  +0.413

for a total  2.528 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 -0.096391,-0.909613,-0.40412 -w ibex-sun -t 2024/12:14:04:01:25

Quaternion    +0.000000,+0.000000,+0.000000,+0.000000

points axis  +1.000000,+0.000000,+0.000000

towards ECI  -0.096391,-0.909613,-0.404120

which is     R.A. +263.951 Decl. -23.836

missing      R.A. +261.697 Decl. -23.198 (ibex-sun)

error is     R.A.   +2.254 Decl.  +0.638

for a total  2.163 deg

 

ibex_rotate -o -u -0.096391,-0.909613,-0.40412 -w ibex-sun -t 2024/12:14:05:36:31

Quaternion    +0.000000,+0.000000,+0.000000,+0.000000

points axis  +1.000000,+0.000000,+0.000000

towards ECI  -0.096391,-0.909613,-0.404120

which is     R.A. +263.951 Decl. -23.836

missing      R.A. +261.769 Decl. -23.202 (ibex-sun)

error is     R.A.   +2.182 Decl.  +0.634

for a total  2.099 deg

 

ibex_rotate -o -u -0.096391,-0.909613,-0.40412 -w ibex-sun -t 2024/12:19:06:16:02

Quaternion    +0.000000,+0.000000,+0.000000,+0.000000

points axis  +1.000000,+0.000000,+0.000000

towards ECI  -0.096391,-0.909613,-0.404120

which is     R.A. +263.951 Decl. -23.836

missing      R.A. +267.232 Decl. -23.394 (ibex-sun)

error is     R.A.   +3.281 Decl.  +0.442

for a total  3.039 deg

 

The Inertial precession maneuver at perigee leaves us pointing in safe directions at the time of the maneuver and at orbit 0672 apogee:

 

ibex_rotate -o -u -0.01443,-0.91346,-0.406673 -w ibex-sun -t 2024/12:19:08:13:34

Quaternion    +0.000000,+0.000000,+0.000000,+0.000000

points axis  +1.000000,+0.000000,+0.000000

towards ECI  -0.014430,-0.913460,-0.406673

which is     R.A. +269.095 Decl. -23.996

missing      R.A. +267.323 Decl. -23.398 (ibex-sun)

error is     R.A.   +1.772 Decl.  +0.598

for a total  1.729 deg

 

ibex_rotate -o -u -0.01443,-0.91346,-0.406673 -w ibex-sun -t 2024-12-24T06:09:20

Quaternion    +0.000000,+0.000000,+0.000000,+0.000000

points axis  +1.000000,+0.000000,+0.000000

towards ECI  -0.014430,-0.913460,-0.406673

which is     R.A. +269.095 Decl. -23.996

missing      R.A. +272.880 Decl. -23.382 (ibex-sun)

error is     R.A.   +3.785 Decl.  +0.614

for a total  3.520 deg

 

There is no overlap with orbit 0670 commands.

 

Command Approval Checklist is attached.

  

Carol

 

-- 

Carol Weaver

University of New Hampshire

503-902-8492

 

From: NIgel Angold <nangold@princeton.edu>
Date: Saturday, November 30, 2024 at 20:42
To: Perry, Timothy E [US] (SP) <Timothy.Perry@ngc.com>
Cc: Carol Weaver <carol.weaver@unh.edu>, Chubin, Eric [US] (SP) <Eric.Chubin@ngc.com>, Coca Gonzales, Andrea [US] (SP) <Andrea.CocaGonzales@ngc.com>, David Heirtzler <David.Heirtzler@unh.edu>, ADS-IBEX@l3harris.com <ADS-IBEX@l3harris.com>, ibexops <IBEXOPS@gmail.com>, isocops <isocops@lists.sr.unh.edu>, kwfairchild <kwfairchild@gmail.com>, Kenneth Fairchild <Ken.Fairchild@unh.edu>, angoldconsulting@earthlink.net <angoldconsulting@earthlink.net>, paul.janzen <Paul.Janzen@mso.umt.edu>, 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: Re: [Isocops] IBEX Orbit #671 ATS Approval (December 10 - 20, 2024)

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_2024_345_o0671a_v001.scr

Nigel

November 27, 2024 at 09:56

 

All, 

   Attached are the planning files for Orbit #671. Please respond to this thread with comments and approvals. Approvals for the Orbit 671 ATS are required by COB, 30 November 2024.

 

 

Please note the following: 

 

Battery Balancing

Eclipse Flag True: 2024/12/19 18:00:00

Eclipse Flag False: 2024/12/19 19:30:00

 

Command Load Constraint Violation Report (CCVR) 

IBEX_2024_345_o0671a_v001.ccvr

# Input files:         1

#   IBEX_2024_345_o0671a_v001.scr

 

==========================

HARD CONSTRAINT VIOLATIONS

==========================

NO VIOLATIONS.

 

==========================

SOFT CONSTRAINT VIOLATIONS

==========================

### The first 2 constraint violations are because of the contact “IBEX,USAK01,ADD,12/19/24,354,23:00:00,12/20/24,355,00:30:00,LAHO 160K IBEX-3 Orbit# 671 SSR_Dump/Tracking Contact/10 Asc” was scheduled for 90 minutes. This is not a problem.

 

IBX-CLC-006: Planned transmission at 2024/12/19 22:58:00 UTC - 2024/12/20

             00:32:00 UTC exceeds the maximum contiguous transmission time of

             5400 seconds

IBX-CLC-015: Battery charge falls below minimum from 2024/12/20 00:17:00 UTC -

             2024/12/20 00:32:00 UTC. Lowest charge level is 7498.840000

             watt-minutes during this interval.

IBX-CLC-016: No command to enable spin pulse protection was found after

             transition to science mode at 2024/12/11 00:35:58 UTC

IBX-CLC-016: No command to enable spin pulse protection was found after

             transition to science mode at 2024/12/14 05:06:31 UTC

 

==============

OTHER MESSAGES

==============

NO MESSAGES.

 

 

Timothy E.Perry

CRS IBEX OCO-2

Mission Operations

timothy.perry@ngc.com

Office (703) 406-5976

IBEX MOC (703)404-7470

Cell (301) 606-1430

 




Please restrict discussions on this email list to non-ITAR sensitive topics.
______________________________________________
Isocops mailing list
Isocops@lists.sr.unh.edu
https://lists.sr.unh.edu/mailman/listinfo/isocops