[Isocops] IBEX Goat Herder for March 3rd & 4th, 2023

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

All,
   The spacecraft is nominal and the inertial maneuver was successful. The orbit 600 ATS and the orbit 601 Hi Gain CAL ATS was uplinked. We had an issue with the first USHI01 contact. We were never able to get a good uplink from the station. After trying for ~30 minutes we ended the contact and scheduled a USAK01 contact from 08:00 – 09:00 GMT. This contact was successful and we saw a good receiver AGC throughout the contact. I also noticed that the Flight computer back orbit buffer was not filling up. I resent the command to enable to Flight computer buffer to start collecting tlm. The FC buffer is incrementing now.

Tasks Accomplished:
CAR # 1297 Orbit 599 Return to science after master Computer Reset
Step # 14 Upload Orbit 600 ATS
  IBEX_2023_063_o0600a_v001 103 commands
CAR 1298 Orbit 601 Hi gain Cal ATS uplink
   IBEX_2023_072_o0601a_v001_hgc
SSR Dump -> Dump New
Enable FC Back orbit tlm

Results from the Inertial Maneuver:
Q1 -0.33849500 ActNor.EstInrToBdy[0]
Q2 0.66359400 ActNor.EstInrToBdy[1]
Q3 -0.44493600 ActNor.EstInrToBdy[2]
Q4 0.49708700 ActNor.EstInrToBdy[3]

GPS sec 1361948173 ActNor.EstTime
UTC time 03/04/2023 06:55:59 output

MPS Diff 0.633 deg

MPS Cmd Vector X 0.962011000
MPS Cmd Vector Y -0.246322000
MPS Cmd Vector Z -0.117728000

CSS Angle TLM 0.727393
CSS Sun-Pointing Angle 1.454786
  03 Mar 23 at 03:30:00

CSS Angle TLM 0.990316
CSS Sun-Pointing Angle 1.980632
  04 Mar 23 at 06:30:00

Pre-Burn
Thruster 1 592 03 Mar 23 at 03:30:00
Thruster 2 592
Thruster 3 768
Thruster 4 768
Post-Burn
Thruster 1 752 04 Mar 23 at 06:30:00
Thruster 2 752
Thruster 3 928
Thruster 4 928
Number of Pulses
Thruster 1 160
Thruster 2 160
Thruster 3 160
Thruster 4 160
Thruster Pairs
Thruster 1 & 2 320
Thruster 3 & 4 320


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