[Isocops] IBEX Goat Herder for 4 May 2022

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

All,
    The apogee contact was nominal and the inertial maneuver was successful.


Results from the Inertial Maneuver:
Q1 -0.60448500 ActNor.EstInrToBdy[0]
Q2 -0.07105330 ActNor.EstInrToBdy[1]
Q3 -0.66857700 ActNor.EstInrToBdy[2]
Q4 0.42726400 ActNor.EstInrToBdy[3]

GPS sec 1335711734 ActNor.EstTime

UTC time 05/04/2022 15:02:00 output
MPS Diff 0.267 deg
MPS Cmd Vector X 0.748350000
MPS Cmd Vector Y 0.612495000
MPS Cmd Vector Z 0.254602000
CSS Angle TLM 1.73068
CSS Sun-Pointing Angle 3.46136
  30 Apr 22 @ 14:30:00
CSS Angle TLM 0.659975
CSS Sun-Pointing Angle 1.31995
  04 May 22 @ 15:00:00
Pre-Burn
Thruster 1 1072 30 Apr 22 @ 14:30:00
Thruster 2 1072
Thruster 3 1184
Thruster 4 1184
Post-Burn
Thruster 1 1360 04 May 22 @ 15:00:00
Thruster 2 1328
Thruster 3 1520
Thruster 4 1552
Number of Pulses
Thruster 1 288
Thruster 2 256
Thruster 3 336
Thruster 4 368
Thruster Pairs
Thruster 1 & 2 544
Thruster 3 & 4 704


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