[Isocops] IBEX Goat Herder for 30 Sept & 01 Oct 2022

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

All,
   The perigee contacts were nominal. The inertial maneuver was successful. We completed CAR #1264 “Hi background test and star sensor tlm cadence” Pass #2. We set the Hi back to normal sweep and increased the star sensor cadence. The SSR was dumped and missing blocks from Orbit #581 was redumped. The Orbit #584 ATS was uplinked. The 18 day timer and FDC totals have been reset to zero.
Note the star tracker is still at 67 percent valid.

Tasks Accomplished:
CAR #1264 Hi background test and star sensor tlm cadence
   Completed Pass #2
CAR #1270 Orbit #584 ATS upload
    IBEX_2022_283_o0584a_v001 88 Cmds
CAR #1268 Dump Orbit 581 Missing Blocks
Reset 18 Day Timer
Reset FDC Totals

Results from the Inertial Maneuver:
Q1 -0.43007700 ActNor.EstInrToBdy[0]
Q2 -0.57585900 ActNor.EstInrToBdy[1]
Q3 0.45871700 ActNor.EstInrToBdy[2]
Q4 0.52249400 ActNor.EstInrToBdy[3]

GPS sec 1348635673 ActNor.EstTime
UTC time 10/01/2022 05:00:59 output

MPS Diff 0.644 deg

MPS Cmd Vector X -0.995830000
MPS Cmd Vector Y -0.079720000
MPS Cmd Vector Z -0.044352000

CSS Angle TLM 0.23239
CSS Sun-Pointing Angle 0.46478
  26 Sept 22 @23:00:00

CSS Angle TLM 0.237388
CSS Sun-Pointing Angle 0.474776
  01 Oct 22 @05:00:00

Pre-Burn
Thruster 1 6480 26 Sept 22 @23:00:00
Thruster 2 6320
Thruster 3 7664
Thruster 4 7824
Post-Burn
Thruster 1 6752 01 Oct 22 @05:00:00
Thruster 2 6592
Thruster 3 7936
Thruster 4 8096
Number of Pulses
Thruster 1 272
Thruster 2 272
Thruster 3 272
Thruster 4 272
Thruster Pairs
Thruster 1 & 2 544

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