[Isocops] IBEX Orbit# 585 ATS Approval (19 Oct 22 - 29 Oct 22)

Carol Weaver Carol.Weaver at unh.edu
Fri Oct 7 12:21:52 EDT 2022


Hi all,
I have looked at the orbit 0585 ATS file, IBEX_2022_292_o0585a_v001.scr and I approve.

The constraint violations in IBEX_2022_292_o0585a_v001.ccvr are from the removal of the ACT_SetSpinPulseProtectEnable Enable commands. The violations are acceptable.

The PL commands in IBEX_2022_292_o0585a_v001.scr match those in the STF, IBEX_2022_292_o0585a_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_292_o0585a_v001.oef and as verified with ibex_orbit.

There is 1 star tracker outage this orbit.  It lasts ~39 hours and ends ~38 hours before the Apogee Sun maneuver.

The ground station command sequences are correct and the timing and bit rates match those in the contacts file, IBEX_Orbit585_Contacts.txt for all contacts (4).

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 0584 left us pointing in safe directions for the orbit 0585 arc A ascending and descending sequences:

ibex_rotate -o -u -0.916321,-0.363741,-0.167474 -w ibex-sun -t 2022/10:20:03:58:55
Quaternion    +0.000000,+0.000000,+0.000000,+0.000000
points axis  +1.000000,+0.000000,+0.000000
towards ECI  -0.916321,-0.363741,-0.167474
which is     R.A. +201.651 Decl.  -9.641
missing      R.A. +204.544 Decl. -10.226 (ibex-sun)
error is     R.A.   +2.893 Decl.  +0.585
for a total  2.910 deg

ibex_rotate -o -u -0.916321,-0.363741,-0.167474 -w ibex-sun -t 2022/10:24:09:01:59
Quaternion    +0.000000,+0.000000,+0.000000,+0.000000
points axis  +1.000000,+0.000000,+0.000000
towards ECI  -0.916321,-0.363741,-0.167474
which is     R.A. +201.651 Decl.  -9.641
missing      R.A. +208.445 Decl. -11.655 (ibex-sun)
error is     R.A.   +6.794 Decl.  +2.014
for a total  6.974 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 +208.516 -d -11.680 -w ibex-sun -t 2022/10:24:10:50:07
Quaternion    +0.000000,+0.000000,+0.000000,+0.000000
points axis  +1.000000,+0.000000,+0.000000
towards ECI  -0.860489,-0.467519,-0.202445
which is     R.A. +208.516 Decl. -11.680
missing      R.A. +208.516 Decl. -11.680 (ibex-sun)
error is     R.A.   +0.000 Decl.  +0.000
for a total  0.000 deg

ibex_rotate -o -r +208.516 -d -11.680  -w ibex-sun -t 2022/10:24:12:20:13
Quaternion    +0.000000,+0.000000,+0.000000,+0.000000
points axis  +1.000000,+0.000000,+0.000000
towards ECI  -0.860489,-0.467519,-0.202445
which is     R.A. +208.516 Decl. -11.680
missing      R.A. +208.575 Decl. -11.700 (ibex-sun)
error is     R.A.   +0.059 Decl.  +0.020
for a total  0.061 deg

ibex_rotate -o -r +208.516 -d -11.680  -w ibex-sun -t 2022/10:28:14:37:28
Quaternion    +0.000000,+0.000000,+0.000000,+0.000000
points axis  +1.000000,+0.000000,+0.000000
towards ECI  -0.860489,-0.467519,-0.202445
which is     R.A. +208.516 Decl. -11.680
missing      R.A. +212.563 Decl. -13.117 (ibex-sun)
error is     R.A.   +4.047 Decl.  +1.437
for a total  4.206 deg

The Inertial precession maneuver at perigee leaves us pointing in safe directions at the time of the maneuver and at orbit 0586 apogee:

ibex_rotate -o -u -0.840662,-0.493233,-0.223624 -w ibex-sun -t 2022/10:28:17:47:45
Quaternion    +0.000000,+0.000000,+0.000000,+0.000000
points axis  +1.000000,+0.000000,+0.000000
towards ECI  -0.840662,-0.493233,-0.223624
which is     R.A. +210.401 Decl. -12.922
missing      R.A. +212.698 Decl. -13.170 (ibex-sun)
error is     R.A.   +2.297 Decl.  +0.248
for a total  2.251 deg

ibex_rotate -o -u -0.840662,-0.493233,-0.223624 -w ibex-sun -t 2022-11-02T14:57:40
Quaternion    +0.000000,+0.000000,+0.000000,+0.000000
points axis  +1.000000,+0.000000,+0.000000
towards ECI  -0.840662,-0.493233,-0.223624
which is     R.A. +210.401 Decl. -12.922
missing      R.A. +217.402 Decl. -14.739 (ibex-sun)
error is     R.A.   +7.001 Decl.  +1.817
for a total  7.036 deg

There is no overlap with orbit 0584 commands.

Command Approval Checklist is attached.

Carol

--
Carol Weaver
University of New Hampshire
503.902.8492

From: Wesley, Sheral R [US] (SP) <Sheral.Wesley at ngc.com>
Date: Thursday, 2022-October-6 at 19:28
To: Perry, Timothy E [US] (SP) <Timothy.Perry at ngc.com>, angoldconsulting <angoldconsulting at earthlink.net>, Carol Weaver <carol.weaver at unh.edu>, Chubin, Eric [US] (SP) <Eric.Chubin at ngc.com>, David Heirtzler <David.Heirtzler at unh.edu>, Kenneth Fairchild <Ken.Fairchild at unh.edu>, IBEXOPS (IBEXOPS at gmail.com) <ibexops at gmail.com>, ADS-IBEX <ads-ibex at l3harris.com>, ISOC <isocops at lists.sr.unh.edu>, Ken Fairchild <kwfairchild at gmail.com>, Paul Janzen <Paul.Janzen at mso.umt.edu>, Tyler, Ryan S [US] (SP) <Ryan.Tyler at ngc.com>, Wesley, Sheral R [US] (SP) <Sheral.Wesley at ngc.com>, Wynn, Reese [US] (SP) <Reese.Wynn at ngc.com>
Subject: IBEX Orbit# 585 ATS Approval (19 Oct 22 - 29 Oct 22)
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,
Please review the following for approval.
Approvals are due by COB  9 Oct  22


  1.  Apogee Sun Maneuver
2022-10-24T10:35:07.000Z,SunMvrBegin,(mvrDuration):900,orbit:585
2022-10-24T10:50:07.000Z,SunMvrEnd,orbit:585



Sheral Wesley  |  Sr Principal Engineer, Satellite Systems

Northrop Grumman Corporation  |  Space Systems

O: 703-406-5641  |  C: 202-236-0802  |  sheral.wesley at ngc.com<mailto:sheral.wesley at ngc.com>

 [cid:1ad9573f-9ee5-4fde-83f8-0a00afc1966f]



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