Hi all,

 

The angle at descending after the apogee Sun maneuver is 3.959 deg.

 

I have looked at the orbit 0624 ATS file, IBEX_2023_281_o0624a_v001.scr and I approve.

 

The constraint violations in IBEX_2023_281_o0624a_v001.ccvr are from the removal of the ACT_SetSpinPulseProtectEnable Enable commands. The violations are acceptable.

 

The PL commands in IBEX_2023_281_o0624a_v001.scr match those in the STF, IBEX_2023_281_o0624a_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_281_o0624a_v001.oef and as verified with ibex_orbit.

 

There is 1 star tracker outage this orbit. Outage begins at 2023-10-10 00:30:09 and lasts for 35.8 hours. 

  

The ground station command sequences are correct and the timing and bit rates match those in the contacts file, IBEX_Orbit624_Contacts.txt for all contacts (4).

 

Battery Balancing is 90 minutes long, more than 2 hours away from payload descending macros, 4.788 hrs, and more than 15 minutes away from a maneuver, 148 mins.

 

The Inertial maneuver at perigee of orbit 0623 left us pointing in safe directions for the orbit 0624 arc A ascending and descending sequences:

 

ibex_rotate -o -u -0.975646,-0.197505,-0.095429 -w ibex-sun -t 2023/10:09:11:21:44

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

points axis  +1.000000,+0.000000,+0.000000

towards ECI  -0.975646,-0.197505,-0.095429

which is     R.A. +191.444 Decl.  -5.476

missing      R.A. +194.373 Decl.  -6.163 (ibex-sun)

error is     R.A.   +2.929 Decl.  +0.687

for a total  2.994 deg

 

ibex_rotate -o -u -0.975646,-0.197505,-0.095429 -w ibex-sun -t 2023/10:13:09:51:53

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

points axis  +1.000000,+0.000000,+0.000000

towards ECI  -0.975646,-0.197505,-0.095429

which is     R.A. +191.444 Decl.  -5.476

missing      R.A. +197.917 Decl.  -7.580 (ibex-sun)

error is     R.A.   +6.473 Decl.  +2.104

for a total  6.766 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 +197.986 -d  -7.607   -w ibex-sun -t 2023/10:13:11:40:01

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

points axis  +1.000000,+0.000000,+0.000000

towards ECI  -0.942761,-0.306067,-0.132377

which is     R.A. +197.986 Decl.  -7.607

missing      R.A. +197.986 Decl.  -7.607 (ibex-sun)

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

for a total  0.000 deg

 

ibex_rotate -o -r +197.986 -d  -7.607  -w ibex-sun -t 2023/10:13:13:10:07

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

points axis  +1.000000,+0.000000,+0.000000

towards ECI  -0.942761,-0.306067,-0.132377

which is     R.A. +197.986 Decl.  -7.607

missing      R.A. +198.043 Decl.  -7.629 (ibex-sun)

error is     R.A.   +0.057 Decl.  +0.022

for a total  0.061 deg

 

ibex_rotate -o -r +197.986 -d  -7.607  -w ibex-sun -t 2023/10:17:10:12:43

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

points axis  +1.000000,+0.000000,+0.000000

towards ECI  -0.942761,-0.306067,-0.132377

which is     R.A. +197.986 Decl.  -7.607

missing      R.A. +201.698 Decl.  -9.085 (ibex-sun)

error is     R.A.   +3.712 Decl.  +1.478

for a total  3.959 deg

 

The Inertial precession maneuver at perigee leaves us pointing in safe directions at the time of the maneuver and at orbit 0625 apogee:

 

ibex_rotate -o -u -0.930464,-0.332477,-0.153934 -w ibex-sun -t 2023/10:17:12:32:22

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

points axis  +1.000000,+0.000000,+0.000000

towards ECI  -0.930464,-0.332477,-0.153934

which is     R.A. +199.663 Decl.  -8.855

missing      R.A. +201.794 Decl.  -9.126 (ibex-sun)

error is     R.A.   +2.131 Decl.  +0.271

for a total  2.122 deg

 

ibex_rotate -o -u -0.930464,-0.332477,-0.153934 -w ibex-sun -t 2023-10-22T09:13:32

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

points axis  +1.000000,+0.000000,+0.000000

towards ECI  -0.930464,-0.332477,-0.153934

which is     R.A. +199.663 Decl.  -8.855

missing      R.A. +206.319 Decl. -10.863 (ibex-sun)

error is     R.A.   +6.656 Decl.  +2.008

for a total  6.858 deg

 

There is no overlap with orbit 0623 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, September 25, 2023 at 12:00
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 #624 ATS Approval ( Oct 09 - 18, 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 products for Orbit #624. Please respond to this thread with comments and approvals. Approvals are required by 16:00gmt 29 Sept 2023 

 

Please note the following: 

1.        Battery Balancing this Orbit. 

Begin 2023/10/17 15:00:00 – End 2023/10/17 16:30:00

The Battery balancing will not take place at perigee since the second perigee contact is at 21:00:00 gmt. The next best quiet time in the orbit was @15:00 – 16:30. This is between the perigee maneuver and the second tracking contact.

 

2.        Command Load Constraint Violation Report (CCVR) 

IBEX_2023_281_o0624a_v001.ccvr

# Input files:         1

#   IBEX_2023_272_o0623a_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 2023/09/30 07:43:58 UTC

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

             transition to science mode at 2023/10/04 12:23:14 UTC

 

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

OTHER MESSAGES

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

NO MESSAGE

 

Timothy E.Perry

CRS IBEX OCO-2

Mission Operations

timothy.perry@ngc.com

Office (703) 406-5976

Cell (301) 606-1430