Hi all,

I have looked at the orbit 0580 ATS file, IBEX_2022_246_o0580a_v001.scr and I approve.

 

The constraint violations in IBEX_2022_246_o0580a_v001.ccvr are from the removal of the ACT_SetSpinPulseProtectEnable Enable commands. The violations are acceptable.

 

The PL commands in IBEX_2022_246_o0580a_v001.scr match those in the STF, IBEX_2022_246_o0580a_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_246_o0580a_v001.oef and as verified with ibex_orbit.

 

There are 2 star tracker outages this orbit. 

  

The ground station command sequences are correct and the timing and bit rates match those in the contacts file, IBEX_Orbit580_Contacts.txt for all contacts (2).

 

No Battery Balancing this orbit.

 

The Inertial maneuver at perigee of orbit 0579 left us pointing in safe directions for the orbit 0580 arc A ascending and descending sequences:

 

ibex_rotate -o -u -0.927839,0.345687,0.140055 -w ibex-sun -t 2022/09:03:15:52:35

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

points axis  +1.000000,+0.000000,+0.000000

towards ECI  -0.927839,+0.345687,+0.140055

which is     R.A. +159.566 Decl.  +8.051

missing      R.A. +162.324 Decl.  +7.480 (ibex-sun)

error is     R.A.   +2.758 Decl.  +0.571

for a total  2.791 deg

 

ibex_rotate -o -u -0.927839,0.345687,0.140055 -w ibex-sun -t 2022/09:07:19:55:07

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

points axis  +1.000000,+0.000000,+0.000000

towards ECI  -0.927839,+0.345687,+0.140055

which is     R.A. +159.566 Decl.  +8.051

missing      R.A. +165.973 Decl.  +6.011 (ibex-sun)

error is     R.A.   +6.407 Decl.  +2.040

for a total  6.678 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 +166.041 -d +5.983 -w ibex-sun -t 2022/09:07:21:43:15

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

points axis  +1.000000,+0.000000,+0.000000

towards ECI  -0.965182,+0.239914,+0.104233

which is     R.A. +166.041 Decl.  +5.983

missing      R.A. +166.041 Decl.  +5.983 (ibex-sun)

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

for a total  0.001 deg

 

ibex_rotate -o -r +166.041 -d +5.983  -w ibex-sun -t 2022/09:07:23:13:21

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

points axis  +1.000000,+0.000000,+0.000000

towards ECI  -0.965182,+0.239914,+0.104233

which is     R.A. +166.041 Decl.  +5.983

missing      R.A. +166.098 Decl.  +5.961 (ibex-sun)

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

for a total  0.061 deg

 

ibex_rotate -o -r +166.041 -d +5.983  -w ibex-sun -t 2022/09:12:04:17:53

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

points axis  +1.000000,+0.000000,+0.000000

towards ECI  -0.965182,+0.239914,+0.104233

which is     R.A. +166.041 Decl.  +5.983

missing      R.A. +170.003 Decl.  +4.314 (ibex-sun)

error is     R.A.   +3.962 Decl.  +1.669

for a total  4.285 deg

 

 

The Sun precession maneuver at perigee leaves us pointing in safe directions at the time of the maneuver and at orbit 0581 apogee:

 

ibex_rotate -o -r +170.204 -d +4.219  -w ibex-sun -t 2022/09:12:09:35:56

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

points axis  +1.000000,+0.000000,+0.000000

towards ECI  -0.982749,+0.169680,+0.073569

which is     R.A. +170.204 Decl.  +4.219

missing      R.A. +170.204 Decl.  +4.219 (ibex-sun)

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

for a total  0.001 deg

 

ibex_rotate -o -r +170.204 -d +4.219  -w ibex-sun -t 2022-09-17T05:06:52

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

points axis  +1.000000,+0.000000,+0.000000

towards ECI  -0.982749,+0.169680,+0.073569

which is     R.A. +170.204 Decl.  +4.219

missing      R.A. +174.396 Decl.  +2.438 (ibex-sun)

error is     R.A.   +4.192 Decl.  +1.781

for a total  4.548 deg

 

There is no overlap with orbit 0579 commands.

 

Command Approval Checklist is attached.

  

Carol

 

-- 

Carol Weaver

University of New Hampshire

503.902.8492

 

From: NIgel Angold <nangold@princeton.edu>
Date: Wednesday, 2022-August-24 at 12:45
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>, David Heirtzler <David.Heirtzler@unh.edu>, IBEX FDG Group <ADS-IBEX@l3harris.com>, IBEXOPS <IBEXOPS@gmail.com>, ISOC <isocops@lists.sr.unh.edu>, Ken Fairchild <fair-play@comcast.net>, Ken Fairchild (kwfairchild@gmail.com) <kwfairchild@gmail.com>, Kenneth Fairchild <Ken.Fairchild@unh.edu>, angoldconsulting <angoldconsulting@earthlink.net>, 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: [Isocops] IBEX Orbit #580 ATS Approval (03 - 12 Sept 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.

 

I approve IBEX_2022_246_o0580a_v001.scr

Nigel


August 22, 2022 at 10:48

All, 

   Attached are the planning files for Orbit #580. Please respond to this thread with comments and approvals.   

Approvals are required by 1800, 24 Aug 2022 

  

Please note the following: 

  1. Apogee Sun Maneuver – 2022/09/07 21:28:15 

 

  1. Perigee Sun Maneuver – 2022/09/12 09:20:56 

 

3.       No Battery Balancing this orbit 

 

4.       Command Load Constraint Violation Report (CCVR) 

IBEX_2022_246_o0580a_v001.ccvr 

#   IBEX_2022_246_o0580a_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 2022/09/03 12:23:39 UTC 

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

             transition to science mode at 2022/09/07 22:43:21 UTC 

 

============== 

OTHER MESSAGES 

============== 

NO MESSAGES. 

  

 



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