Hi all,

The angle at descending after the apogee sun maneuver is 3.996 deg.

 

I have looked at the orbit 0670 ATS file, IBEX_2024_336_o0670a_v001.scr and I approve.

 

The constraint violations in IBEX_2024_336_o0670a_v001.ccvr are from the removal of the ACT_SetSpinPulseProtectEnable Enable commands. The violations are acceptable.

 

The PL commands in IBEX_2024_336_o0670a_v001.scr match those in the STF, IBEX_2024_336_o0670a_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_336_o0670a_v001.oef and as verified with ibex_orbit.

 

There is 1 star tracker outage this orbit. Outage begins at 2024-12-04 06:16:27 and lasts for 107.7 hours. 

  

The ground station command sequences are correct and the timing and bit rates match those in the contacts file, IBEX_Orbit670_Contacts.txt for all contacts (3).

 

Battery Balancing is 90 minutes long, more than 2 hours away from payload descending macros, 10.816 hrs, and more than 15 minutes away from a maneuver, 534 mins.

 

The Inertial maneuver at perigee of orbit 0669 left us pointing in safe directions for the orbit 0670 arc A ascending and descending sequences:

 

ibex_rotate -o -u -0.360187,-0.852227,-0.37944 -w ibex-sun -t 2024/12:02:01:48:56

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

points axis  +1.000000,+0.000000,+0.000000

towards ECI  -0.360187,-0.852227,-0.379440

which is     R.A. +247.089 Decl. -22.299

missing      R.A. +248.429 Decl. -21.971 (ibex-sun)

error is     R.A.   +1.340 Decl.  +0.328

for a total  1.284 deg

 

ibex_rotate -o -u -0.360187,-0.852227,-0.37944 -w ibex-sun -t 2024/12:06:00:25:59

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

points axis  +1.000000,+0.000000,+0.000000

towards ECI  -0.360187,-0.852227,-0.379440

which is     R.A. +247.089 Decl. -22.299

missing      R.A. +252.716 Decl. -22.459 (ibex-sun)

error is     R.A.   +5.627 Decl.  +0.160

for a total  5.205 deg

 

 

The Sun 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 -r +252.796 -d -22.467 -w ibex-sun -t 2024/12:06:02:14:07

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

points axis  +1.000000,+0.000000,+0.000000

towards ECI  -0.273325,-0.882753,-0.382151

which is     R.A. +252.796 Decl. -22.467

missing      R.A. +252.796 Decl. -22.467 (ibex-sun)

error is     R.A.   +0.000 Decl.  +0.000

for a total  0.000 deg

 

ibex_rotate -o -r +252.796 -d -22.467 -w ibex-sun -t 2024/12:06:03:44:13

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

points axis  +1.000000,+0.000000,+0.000000

towards ECI  -0.273325,-0.882753,-0.382151

which is     R.A. +252.796 Decl. -22.467

missing      R.A. +252.864 Decl. -22.474 (ibex-sun)

error is     R.A.   +0.068 Decl.  +0.007

for a total  0.063 deg

 

ibex_rotate -o -r +252.796 -d -22.467 -w ibex-sun -t 2024/12:10:02:11:02

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

points axis  +1.000000,+0.000000,+0.000000

towards ECI  -0.273325,-0.882753,-0.382151

which is     R.A. +252.796 Decl. -22.467

missing      R.A. +257.103 Decl. -22.888 (ibex-sun)

error is     R.A.   +4.307 Decl.  +0.421

for a total  3.996 deg

 

The Inertial precession maneuver at perigee leaves us pointing in safe directions at the time of the maneuver and at orbit 0671 apogee:

 

ibex_rotate -o -u -0.176393,-0.899168,-0.400477 -w ibex-sun -t 2024/12:10:04:05:33

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. +257.192 Decl. -22.898 (ibex-sun)

error is     R.A.   +1.709 Decl.  +0.710

for a total  1.724 deg

 

ibex_rotate -o -u -0.176393,-0.899168,-0.400477 -w ibex-sun -t 2024-12-15T03:51:23

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. +262.780 Decl. -23.242 (ibex-sun)

error is     R.A.   +3.879 Decl.  +0.366

for a total  3.578 deg

 

There is no overlap with orbit 0669 commands.

 

Command Approval Checklist is attached.

  

Carol

 

-- 

Carol Weaver

University of New Hampshire

503-902-8492

 

From: NIgel Angold <nangold@princeton.edu>
Date: Friday, November 22, 2024 at 01:22
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>, 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: IBEX Orbit #670 ATS Approval (December 01 - 10, 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_336_o0670a_v001.scr

Nigel

November 17, 2024 at 17:58

All, 

   Attached are the planning files for Orbit #670. Please respond to this thread with comments and approvals. Approvals for the Orbit 670 ATS are required by COB, 21 November 2024.

 

 

Please note the following: 

 

Battery Balancing

Eclipse Flag True: 2024/12/10 13:00:00

Eclipse Flag False: 2024/12/10 14:30:00

 

Command Load Constraint Violation Report (CCVR) 

IBEX_2024_336_o0670a_v001.ccvr

# Input files:         1

#   IBEX_2024_336_o0670a_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 2024/12/02 00:37:40 UTC

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

             transition to science mode at 2024/12/06 03:14:13 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