Hi all,

 

The angle of decending after the apogee sun maneuver is 4.032 deg.

 

I have looked at the orbit 0630 ATS file, IBEX_2023_336_o0630a_v001.scr and I approve.

 

The constraint violations in IBEX_2023_336_o0630a_v001.ccvr are from the removal of the ACT_SetSpinPulseProtectEnable Enable commands. The violations are acceptable.

 

The PL commands in IBEX_2023_336_o0630a_v001.scr match those in the STF, IBEX_2023_336_o0630a_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_336_o0630a_v001.oef and as verified with ibex_orbit.

 

There is 1 star tracker outage this orbit. Outage begins at 2023-12-04 04:05:48 and lasts for 115.2 hours. 

  

The ground station command sequences are correct and the timing and bit rates match those in the contacts file, IBEX_Orbit630_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 0629 left us pointing in safe directions for the orbit 0630 arc A ascending and descending sequences:

 

ibex_rotate -o -u -0.362113,-0.851554,-0.379117 -w ibex-sun -t 2023/12:02:17:00:09

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

points axis  +1.000000,+0.000000,+0.000000

towards ECI  -0.362113,-0.851554,-0.379117

which is     R.A. +246.963 Decl. -22.279

missing      R.A. +248.305 Decl. -21.959 (ibex-sun)

error is     R.A.   +1.342 Decl.  +0.320

for a total  1.283 deg

 

ibex_rotate -o -u -0.362113,-0.851554,-0.379117 -w ibex-sun -t 2023/12:06:16:28:42

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

points axis  +1.000000,+0.000000,+0.000000

towards ECI  -0.362113,-0.851554,-0.379117

which is     R.A. +246.963 Decl. -22.279

missing      R.A. +252.619 Decl. -22.456 (ibex-sun)

error is     R.A.   +5.656 Decl.  +0.177

for a total  5.234 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 +252.700 -d -22.464 -w ibex-sun -t 2023/12:06:18:16:50

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

points axis  +1.000000,+0.000000,+0.000000

towards ECI  -0.274810,-0.882313,-0.382103

which is     R.A. +252.700 Decl. -22.464

missing      R.A. +252.700 Decl. -22.464 (ibex-sun)

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

for a total  0.000 deg

 

ibex_rotate -o -r +252.700 -d -22.464 -w ibex-sun -t 2023/12:06:19:46:56

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

points axis  +1.000000,+0.000000,+0.000000

towards ECI  -0.274810,-0.882313,-0.382103

which is     R.A. +252.700 Decl. -22.464

missing      R.A. +252.767 Decl. -22.471 (ibex-sun)

error is     R.A.   +0.067 Decl.  +0.007

for a total  0.062 deg

 

ibex_rotate -o -r +252.700 -d -22.464 -w ibex-sun -t 2023/12:10:18:53:23

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

points axis  +1.000000,+0.000000,+0.000000

towards ECI  -0.274810,-0.882313,-0.382103

which is     R.A. +252.700 Decl. -22.464

missing      R.A. +257.046 Decl. -22.883 (ibex-sun)

error is     R.A.   +4.346 Decl.  +0.419

for a total  4.032 deg

The Inertial precession maneuver at perigee leaves us pointing in safe directions at the time of the maneuver and at orbit 0631 apogee:

 

 ibex_rotate -o -u -0.17728,-0.898951,-0.400573 -w ibex-sun -t 2023/12:10:21:08:56

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

points axis  +1.000000,+0.000000,+0.000000

towards ECI  -0.177280,-0.898951,-0.400573

which is     R.A. +258.844 Decl. -23.614

missing      R.A. +257.153 Decl. -22.896 (ibex-sun)

error is     R.A.   +1.691 Decl.  +0.718

for a total  1.712 deg

 

ibex_rotate -o -u -0.17728,-0.898951,-0.400573 -w ibex-sun -t 2023-12-15T19:25:15

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

points axis  +1.000000,+0.000000,+0.000000

towards ECI  -0.177280,-0.898951,-0.400573

which is     R.A. +258.844 Decl. -23.614

missing      R.A. +262.665 Decl. -23.246 (ibex-sun)

error is     R.A.   +3.821 Decl.  +0.368

for a total  3.525 deg

 

There is an overlap with the contact commands in Orbit 0629. This is acceptable.

 

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: Saturday, November 18, 2023 at 17:03
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>, 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 #630 ATS Approval ( Dec 02 - 11, 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.

 

All, 

   Attached are the planning files for Orbit #630. Please respond to this thread with comments and approvals. Approvals are required by COB 26 Nov 2023.

 

Please note the following: 

 

1.        Battery Balancing

Eclipse Flag True: 2023/12:11:06:00:00

Eclipse Flag False: 2023/12:11:07:30:00

 

2.        Command Load Constraint Violation Report (CCVR) 

IBEX_2023_336_o0630a_v001.ccvr

# Input files:         1

#   IBEX_2023_336_o0630a_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 2023/12/02 15:26:50 UTC

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

             transition to science mode at 2023/12/06 19:16:56 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