[Isocops] IBEX Goat Herder for 10 & 11 May 2020

[Nigel Angold]

Thanks Tim.

This demonstrates the flexibility of our new operations strategy. Appreciated.

Nigel

> All,
>     The perigee contacts were nominal for CMD and TLM. The Inertial maneuver was successful.
> The Instrument ATS for orbit #488 was uploaded during the USAK01 contact on 11 May @00:30gmt.
> Total commands on board at LOS were 228. The Master reset timer reset command executed @01:15:00 and was verified @01:25:00.
>  
> Note: the ATS’s for orbit#490 will be sent out on 11 May.
>  
> The following was accomplished:
> Reset FDC Totals
> Set Spacecraft Time
> SSR Dump -> Dump New
> CAR# 1096 ATS upload -> IBEX_2020_140_o0488a_INST_V001 46 Cmds
>  
> Results from the Inertial Maneuver:
>  
> Q1 0.09546380 ActNor.EstInrToBdy[0]
> Q2 0.58523000 ActNor.EstInrToBdy[1]
> Q3 0.65442300 ActNor.EstInrToBdy[2]
> Q4 0.46910200 ActNor.EstInrToBdy[3]
> GPS sec 1273192202 ActNor.EstTime
> UTC time 05/11/2020 00:29:48 output
> MPS Cmd Vector X 0.669273000
> MPS Cmd Vector Y 0.685255000
> MPS Cmd Vector Z 0.287227000
> MPS Diff 0.791 deg
> CSS Angle TLM 0.359365 
> CSS Sun-Pointing Angle 0.71873 
>   06 May 20 @ 03:00
> CSS Angle TLM 0.359909 
> CSS Sun-Pointing Angle 0.719818 
>   11 May 20 @ 00:30
> Pre-Burn   
> Thruster 1 8672 06 May 20 @ 03:00
> Thruster 2 8400 
> Thruster 3 11216 
> Thruster 4 11488 
> Post-Burn   
> Thruster 1 8928 11 May 20 @ 00:30
> Thruster 2 8656 
> Thruster 3 11488 
> Thruster 4 11760 
> Number of Pulses   
> Thruster 1 256 
> Thruster 2 256 
> Thruster 3 272 
> Thruster 4 272 
> Thruster Pairs  
> Thruster 1 & 2 512 
> Thruster 3 & 4 544 
>  
>  
>  
>  
> Timothy E. Perry
> Mission Operations
> CRS, IBEX, OCO-2 & TESS
> timothy.perry at ngc.com <mailto:timothy.perry at ngc.com>
> Office (703) 406-5976
> Cell (301) 606-1430
>  
> <image002.png>
>  

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