[Isocops] IBEX Goat Herder for 29 Feb 2020

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

All,
    The perigee contacts were nominal for CMD and TLM. The Inertial maneuver was successful.

The following was accomplished:
SSR Dump -> Dump new & reset pointers
Reset Master Timer
Set Spacecraft Clock
CAR #1086 ATS upload -> IBEX_2020_069_o0480a_V001 93 Cmds
Reset FDC Totals


Results from the Inertial Maneuver:
Q1 0.32760500 ActNor.EstInrToBdy[0]
Q2 0.67537000 ActNor.EstInrToBdy[1]
Q3 0.09292420 ActNor.EstInrToBdy[2]
Q4 0.65415200 ActNor.EstInrToBdy[3]
MPS Cmd Vector X 0.945157000
MPS Cmd Vector Y -0.295488000
MPS Cmd Vector Z -0.139156000
GPS sec 1266970192 ActNor.EstTime
UTC time 02/29/2020 00:09:38 output
MPS Diff 0.829 deg
CSS Angle TLM 0.625263
CSS Sun-Pointing Angle 1.250526
  26 Feb 20 @ 18:00
CSS Angle TLM 0.696893
CSS Sun-Pointing Angle 1.393786
  29 Feb 20 @ 00:05
Pre-Burn
Thruster 1 4768 26 Feb 20 @ 18:00
Thruster 2 4624
Thruster 3 6384
Thruster 4 6528
Post-Burn
Thruster 1 5040 29 Feb 20 @ 00:05
Thruster 2 4896
Thruster 3 6704
Thruster 4 6848
Number of Pulses
Thruster 1 272
Thruster 2 272
Thruster 3 320
Thruster 4 320
Thruster Pairs
Thruster 1 & 2 544
Thruster 3 & 4 640


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

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