[Isocops] Goat Herder for 1 Feb 2019

[Perry, Timothy]

All,
    The Perigee contacts were nominal for CMD and TLM. The Inertial maneuver was successful.
The following was performed during these contacts:
CAR 1020 Dump orbit 435 SSR data and reset read write pointers to test bad SSR block locations
Per formed an SSR Dump new on the first pass then set the pointers to 5600 and dumped the FC Backorbit data.
On the second pass we performed another SSR dump for locations 5600 - 6268.and dumped the FC backorbit data again.
CAR 1021 ATS uplink - IBEX_2019_041_o0437a_v001 86 cmds
Reset master timer
Dumped FC Back Orbit data 2 times
Set SC Clock
Rest FDC Totals

Inertial Maneuver results:
Q1 -0.19985000
Q2 0.77739900
Q3 -0.50978600
Q4 0.30956300
GPS sec 1233036573.000 ActNor.EstTime
MPS Cmd Vector X 0.686208000
MPS Cmd Vector Y -0.663266000
MPS Cmd Vector Z -0.298658000
MPS Diff 0.665 deg
CSS Angle TLM 1.36444
CSS Sun-Pointing Angle 2.72888
  27 Jan 19 @17:00
CSS Angle TLM 0.30066
CSS Sun-Pointing Angle 0.60132
  1 Feb 19 @06:00
Pre-Burn
Thruster 1 5072 27 Jan 19 @17:00
Thruster 2 4976
Thruster 3 6080
Thruster 4 6176
Post-Burn
Thruster 1 5408 1 Feb 19 @06:00
Thruster 2 5264
Thruster 3 6416
Thruster 4 6560
Number of Pulses 0
Thruster 1 336
Thruster 2 288
Thruster 3 336
Thruster 4 384
Thruster Pairs
Thruster 1 & 2 624
Thruster 3 & 4 720




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

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