[Isocops] Goat Herder for 18 Feb 23 "Flight Computer Reset"

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

All,

    During the apogee contact the flight computer reset @15:14:41. Prior to the reset the apogee inertial maneuver was successful. We do show the CEU 5 Volt is on and the payload has been safed. I have scheduled the following contact for later today: USHI02 02/18/23 049 18:00:00 - 19:30:00. This contact will be used to recover the spacecraft bus and the next available time will be on 21 Feb. We will recover the payload at that time. I will post the new time when they have been scheduled.





Results from the Inertial Maneuver:
Q1 0.46119300 ActNor.EstInrToBdy[0]
Q2 0.61936900 ActNor.EstInrToBdy[1]
Q3 0.10152500 ActNor.EstInrToBdy[2]
Q4 0.62719700 ActNor.EstInrToBdy[3]

GPS sec 1360767681 ActNor.EstTime

UTC time 02/18/2023 15:01:07 output
MPS Diff 0.727 deg
MPS Cmd Vector X 0.871664000
MPS Cmd Vector Y -0.445957000
MPS Cmd Vector Z -0.203283000
CSS Angle TLM 0.776069
CSS Sun-Pointing Angle 1.552138
  14 Feb 23 at 03:00:00
CSS Angle TLM 1.94269
CSS Sun-Pointing Angle 3.88538
  18 Feb 23 at 15:00:00
Pre-Burn
Thruster 1 1168 14 Feb 23 at 03:00:00
Thruster 2 1168
Thruster 3 1840
Thruster 4 1840
Post-Burn
Thruster 1 1488 18 Feb 23 at 15:00:00
Thruster 2 1440
Thruster 3 2160
Thruster 4 2208
Number of Pulses
Thruster 1 320
Thruster 2 272
Thruster 3 320
Thruster 4 368
Thruster Pairs
Thruster 1 & 2 592
Thruster 3 & 4 688


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