Hi all,
I can redo the predicts with the updated maneuvers. Nigel, to clarify, are you wanting an updating star tracker outage report?
I will just need to know whether the perigee inertial maneuver was executed or not – which sounds like the same question that was stated below regarding whether we had any pulses for it.
Thanks!
Kayton
Kayton Lane
Astrodynamics Engineer
Space & airborne systems / L3HARRIS TECHNOLOGIES
w +1 321 729 1809
m +1 218 431 0586
L3Harris.com / Kayton.Lane@L3Harris.com
Palm Bay, FL 32905 / USA
From: Nigel Angold <nangold@princeton.edu>
Sent: Monday, April 3, 2023 7:59 AM
To: Perry, Timothy E [US] (SP) <Timothy.Perry@ngc.com>
Cc: bhautama@gmail.com; carol.weaver@unh.edu; Chubin, Eric [US] (SP) <Eric.Chubin@ngc.com>; SM[SSTC] - ADS-IBEX <ADS-IBEX@L3Harris.com>; IBEXOPS@gmail.com; isocops@lists.sr.unh.edu; fair-play@comcast.net; kwfairchild@gmail.com; ken.fairchild@unh.edu; Leonard, Benjamin Y [US] (SP) <Benjamin.Leonard@ngc.com>; angoldconsulting@earthlink.net; 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: [EXTERNAL] Re: IBEX Goat Herder for 3 April 2023
WARNING: Email originated from an EXTERNAL source. Do NOT click links, open attachments or reply unless you recognize sender and know the content is safe.
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?
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@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
Office (703) 406-5976
Cell (301) 606-1430
CONFIDENTIALITY NOTICE: This email and any attachments are for the sole use of the intended recipient and may contain material that is proprietary, confidential, privileged or otherwise legally protected or restricted under applicable government laws. Any review, disclosure, distributing or other use without expressed permission of the sender is strictly prohibited. If you are not the intended recipient, please contact the sender and delete all copies without reading, printing, or saving.