[Isocops] IBEX Goat Herder for 29 March 2022

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

All,
   The apogee contact was nominal. The inertial maneuver was successful. The Orbit 563 ATS was uplinked.

Tasks Accomplished:
Reset FDC Totals
CAR 1234 Orbit #563 ATS uplink
    IBEX _2022_093_o0563a_v001 93 cmds


Results from the Inertial Maneuver:
Q1 -0.04821150 ActNor.EstInrToBdy[0]
Q2 0.68997500 ActNor.EstInrToBdy[1]
Q3 0.01905210 ActNor.EstInrToBdy[2]
Q4 0.72197500 ActNor.EstInrToBdy[3]

GPS sec 1332597776 ActNor.EstTime

UTC time 03/29/2022 14:02:42 output
MPS Diff 0.668 deg
MPS Cmd Vector X 0.994210000
MPS Cmd Vector Y 0.102145000
MPS Cmd Vector Z 0.033365000
CSS Angle TLM 0.370623
CSS Sun-Pointing Angle 0.741246
  25 Mar 22 @03:00:00
CSS Angle TLM 0.310274
CSS Sun-Pointing Angle 0.620548
  29 Mar 22 @14:00:00
Pre-Burn
Thruster 1 18656 25 Mar 22 @03:00:00
Thruster 2 18144
Thruster 3 23776
Thruster 4 24288
Post-Burn
Thruster 1 18960 29 Mar 22 @14:00:00
Thruster 2 18400
Thruster 3 24064
Thruster 4 24624
Number of Pulses
Thruster 1 304
Thruster 2 256
Thruster 3 288
Thruster 4 336
Thruster Pairs
Thruster 1 & 2 560
Thruster 3 & 4 624


-------------- next part --------------
An HTML attachment was scrubbed...
URL: <https://lists.sr.unh.edu/pipermail/isocops/attachments/20220329/99ad696c/attachment.html>