Hi all,

The angle at descending after the sun procession maneuver is 4.070 deg.

 

I have looked at the orbit 0667 ATS file, IBEX_2024_308_o0667a_v001.scr and I approve.

 

The constraint violations in IBEX_2024_308_0667_v001.ccvr are from the removal of the ACT_SetSpinPulseProtectEnable Enable commands. The violations are acceptable.

 

The PL commands in IBEX_2024_308_o0667a_v001.scr match those in the STF, IBEX_2024_308_o0667a_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_308_o0667a_v001.oef and as verified with ibex_orbit.

 

There is 1 star tracker outage this orbit. Outage begins at 2024-11-05 02:28:27 and lasts for 110.7 hours. 

  

The ground station command sequences are correct and the timing and bit rates match those in the contacts file, IBEX_Orbit667_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 0666 left us pointing in safe directions for the orbit 0667 arc A ascending and descending sequences:

 

 ibex_rotate -o -u -0.775356,-0.575809,-0.259358 -w ibex-sun -t 2024/11:04:09:39:13

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

points axis  +1.000000,+0.000000,+0.000000

towards ECI  -0.775356,-0.575809,-0.259358

which is     R.A. +216.599 Decl. -15.032

missing      R.A. +219.709 Decl. -15.498 (ibex-sun)

error is     R.A.   +3.110 Decl.  +0.466

for a total  3.037 deg

 

ibex_rotate -o -u -0.775356,-0.575809,-0.259358 -w ibex-sun -t 2024/11:08:10:11:46

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

points axis  +1.000000,+0.000000,+0.000000

towards ECI  -0.775356,-0.575809,-0.259358

which is     R.A. +216.599 Decl. -15.032

missing      R.A. +223.680 Decl. -16.642 (ibex-sun)

error is     R.A.   +7.081 Decl.  +1.610

for a total  7.000 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 +223.757 -d -16.663   -w ibex-sun -t 2024/11:08:12:03:12

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

points axis  +1.000000,+0.000000,+0.000000

towards ECI  -0.691949,-0.662559,-0.286742

which is     R.A. +223.757 Decl. -16.663

missing      R.A. +223.757 Decl. -16.663 (ibex-sun)

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

for a total  0.000 deg

 

ibex_rotate -o -r +223.757 -d -16.663 -w ibex-sun -t 2024/11:08:13:30:00

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

points axis  +1.000000,+0.000000,+0.000000

towards ECI  -0.691949,-0.662559,-0.286742

which is     R.A. +223.757 Decl. -16.663

missing      R.A. +223.817 Decl. -16.680 (ibex-sun)

error is     R.A.   +0.060 Decl.  +0.017

for a total  0.060 deg

 

ibex_rotate -o -r +223.757 -d -16.663  -w ibex-sun -t 2024/11:12:13:34:20

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

points axis  +1.000000,+0.000000,+0.000000

towards ECI  -0.691949,-0.662559,-0.286742

which is     R.A. +223.757 Decl. -16.663

missing      R.A. +227.850 Decl. -17.797 (ibex-sun)

error is     R.A.   +4.093 Decl.  +1.134

for a total  4.070 deg

 

The Inertial precession maneuver at perigee leaves us pointing in safe directions at the time of the maneuver and at orbit 0668 apogee:

 

ibex_rotate -o -u -0.664446,-0.682073,-0.305429 -w ibex-sun -t 2024/11:12:15:32:37

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

points axis  +1.000000,+0.000000,+0.000000

towards ECI  -0.664446,-0.682073,-0.305429

which is     R.A. +225.750 Decl. -17.784

missing      R.A. +227.937 Decl. -17.823 (ibex-sun)

error is     R.A.   +2.187 Decl.  +0.039

for a total  2.082 deg

 

ibex_rotate -o -u -0.664446,-0.682073,-0.305429 -w ibex-sun -t 2024-11-17T17:48:47

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

points axis  +1.000000,+0.000000,+0.000000

towards ECI  -0.664446,-0.682073,-0.305429

which is     R.A. +225.750 Decl. -17.784

missing      R.A. +233.200 Decl. -19.116 (ibex-sun)

error is     R.A.   +7.450 Decl.  +1.332

for a total  7.191 deg

 

There is no overlap with orbit 0666 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: Monday, October 21, 2024 at 10:28
To: 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@gmail.com <IBEXOPS@gmail.com>, isocops@lists.sr.unh.edu <isocops@lists.sr.unh.edu>, 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 #667 ATS Approval (November 04 - 13, 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.

 

 

All, 

   Attached are the planning files for Orbit #667. Please respond to this thread with comments and approvals. Approvals for the Orbit 667 ATS are required by COB, 24 October 2024.

 

 

Please note the following: 

 

Battery Balancing

Eclipse Flag True: 2024/11/13 01:00:00

Eclipse Flag False: 2024/11/13 02:30:00

 

Command Load Constraint Violation Report (CCVR) 

IBEX_2024_308_0667_v001.ccvr

# Input files:         1

#   IBEX_2024_308_o0667a_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 2024/11/04 08:23:15 UTC

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

             transition to science mode at 2024/11/08 13:00:00 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