Hi all,

I have looked at the orbit 0562 ATS file, IBEX_2022_083_o0562a_v001.scr and I approve.

 

The constraint violations in IBEX_2022_083_o0562a_v001.ccvr are from the removal of the ACT_SetSpinPulseProtectEnable Enable commands. The violations are acceptable.

 

The PL commands in IBEX_2022_083_o0562a_v001.scr match those in the STF, IBEX_2022_083_o0562a_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_2022_083_o0562a_v001.oef and as verified with ibex_orbit.

 

There is 1 star tracker outage this orbit lasting ~4.5 hours and ending ~5.3 hours before the perigee maneuver.

 

The ground station command sequences are correct and the timing and bit rates match those in the contacts file, IBEX_Orbit562_Contacts.txt for all contacts (2).

 

No Battery Balancing this orbit.

 

The Inertial maneuver at perigee of orbit 0561 left us pointing in safe directions for the orbit 0562 arc A ascending and descending sequences:

 

ibex_rotate -o -u 0.999527,0.030573,0.003438 -w ibex-sun -t 2022/03:25:07:53:53

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

points axis  +1.000000,+0.000000,+0.000000

towards ECI  +0.999527,+0.030573,+0.003438

which is     R.A.   +1.752 Decl.  +0.197

missing      R.A.   +3.965 Decl.  +1.697 (ibex-sun)

error is     R.A.   +2.213 Decl.  +1.500

for a total  2.673 deg

 

ibex_rotate -o -u 0.999527,0.030573,0.003438 -w ibex-sun -t 2022/03:29:00:29:17

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

points axis  +1.000000,+0.000000,+0.000000

towards ECI  +0.999527,+0.030573,+0.003438

which is     R.A.   +1.752 Decl.  +0.197

missing      R.A.   +7.431 Decl.  +3.212 (ibex-sun)

error is     R.A.   +5.679 Decl.  +3.015

for a total  6.427 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 0.99421,0.102145,0.033365 -w ibex-sun -t 2022/03:29:02:12:25

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

points axis  +1.000000,+0.000000,+0.000000

towards ECI  +0.994210,+0.102145,+0.033365

which is     R.A.   +5.866 Decl.  +1.912

missing      R.A.   +7.496 Decl.  +3.242 (ibex-sun)

error is     R.A.   +1.630 Decl.  +1.330

for a total  2.103 deg

 

ibex_rotate -o -u 0.99421,0.102145,0.033365 -w ibex-sun -t 2022/03:29:03:47:31

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

points axis  +1.000000,+0.000000,+0.000000

towards ECI  +0.994210,+0.102145,+0.033365

which is     R.A.   +5.866 Decl.  +1.912

missing      R.A.   +7.557 Decl.  +3.269 (ibex-sun)

error is     R.A.   +1.691 Decl.  +1.357

for a total  2.166 deg

 

ibex_rotate -o -u 0.99421,0.102145,0.033365 -w ibex-sun -t 2022/04:02:14:59:25

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

points axis  +1.000000,+0.000000,+0.000000

towards ECI  +0.994210,+0.102145,+0.033365

which is     R.A.   +5.866 Decl.  +1.912

missing      R.A.  +11.526 Decl.  +4.964 (ibex-sun)

error is     R.A.   +5.660 Decl.  +3.052

for a total  6.421 deg

 

The Inertial precession maneuver at perigee leaves us pointing in safe directions at the time of the maneuver and at orbit 0563 apogee:

 

ibex_rotate -o -u 0.982755,0.173039,0.065194 -w ibex-sun -t 2022/04:02:18:45:04

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

points axis  +1.000000,+0.000000,+0.000000

towards ECI  +0.982755,+0.173039,+0.065194

which is     R.A.   +9.986 Decl.  +3.738

missing      R.A.  +11.663 Decl.  +5.015 (ibex-sun)

error is     R.A.   +1.677 Decl.  +1.277

for a total  2.104 deg

 

ibex_rotate -o -u 0.982755,0.173039,0.065194 -w ibex-sun -t 2022-04-07T14:44:28

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

points axis  +1.000000,+0.000000,+0.000000

towards ECI  +0.982755,+0.173039,+0.065194

which is     R.A.   +9.986 Decl.  +3.738

missing      R.A.  +16.181 Decl.  +6.900 (ibex-sun)

error is     R.A.   +6.195 Decl.  +3.162

for a total  6.931 deg

 

There is no overlap with orbit 0561 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: Friday, 2022-March-11 at 10:54
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>, fair-play@comcast.net <fair-play@comcast.net>, 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 #562 ATS Approval (24 Mar – 03 Apr 2022)

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 #562. Please respond to this thread with comments and approvals.  

Approvals are required by COB, 14 Mar 2022

 

Please note the following:

  1. No Battery Balancing this orbit

 

  1. Command Load Constraint Violation Report (CCVR)

IBEX_2022_083_o0562a_v001.ccvr

# Input files:         1

#   IBEX_2022_083_o0562a_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 2022/03/25 04:36:31 UTC

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

             transition to science mode at 2022/03/29 03:17:31 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