[Isocops] IBEX Goat Herder for 3 April 2023

[Perry, Timothy E [US] (SP)]

From: Nigel Angold <nangold at princeton.edu>
Sent: Monday, April 3, 2023 7:59 AM
To: Perry, Timothy E [US] (SP) <Timothy.Perry at ngc.com>
Cc: bhautama at gmail.com; carol.weaver at unh.edu; Chubin, Eric [US] (SP) <Eric.Chubin at ngc.com>; ADS-IBEX at l3harris.com; IBEXOPS at gmail.com; isocops at lists.sr.unh.edu; fair-play at comcast.net; kwfairchild at gmail.com; ken.fairchild at unh.edu; Leonard, Benjamin Y [US] (SP) <Benjamin.Leonard at ngc.com>; angoldconsulting at earthlink.net; 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: EXT :Re: IBEX Goat Herder for 3 April 2023

Thanks, Tim and Ken for working this.

Is there any chance that we were in a partial outage because of the failed maneuver followed by the Sun pointing maneuver instead of the inertial? I’m not sure if that would explain the percent valid bouncing around  like that. But it’s odd that the value was back up to a solid 78-80% last contact.

Did we have any pulses for the failed maneuver? We did have a partial maneuver. Here were the pulse counts
Pre-Burn
Thruster 1 2016 26 Mar 23 at 12:00:00
Thruster 2 1936
Thruster 3 2224
Thruster 4 2304
Post-Burn
Thruster 1 2240 31 Mar 23 at 18:00:00
Thruster 2 2160
Thruster 3 2464
Thruster 4 2544
Number of Pulses
Thruster 1 224
Thruster 2 224
Thruster 3 240
Thruster 4 240
Thruster Pairs
Thruster 1 & 2 448
Thruster 3 & 4 480


Would FD running the predicts with the actual attitudes be useful/possible?

Thanks,
Nigel
Sent from my iPhone


On Apr 3, 2023, at 4:13 AM, Perry, Timothy E [US] (SP) <Timothy.Perry at ngc.com<mailto:Timothy.Perry at ngc.com>> wrote:


All,

   The contact was successful. We were able to delete all the timed commands and uplink a new Orbit 603 ATS version 2. On previous contacts we were seeing the star tracker percent valid value jump around from 0 – 80. That was what caused the spacecraft to go into contingence mode during the perigee inertial maneuver. This contact the star tracker percent valid was stable between 78 & 80.



Tasks Accomplished:

Ops Procedure OP924-31423 Delete timed commands

CAR # 1307 Orbit 603 Version 2 ATS uplink

Reset FDC Totals




Timothy E.Perry
CRS IBEX OCO-2
Mission Operations
timothy.perry at ngc.com<mailto:timothy.perry at ngc.com>
Office (703) 406-5976
Cell (301) 606-1430

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