[Isocops] IBEX Goat Herder 26 Jan 11
Ibex Mission Operations
ibexops at gmail.com
Thu Jan 27 21:49:41 EST 2011
Guys,
The perigee contacts for Orbit# 110 were nominal for command/telemetry
and doppler data.
Data was collected from the SSR, FC and remaining 40 blocks in ORbit# 106
See attached Goat Herder for additional information
--
Sheral R. Wesley
SPVR., Satellite Operations
IBEX Mission OPS
(304) 279-6678
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IBEX Goat Herder 26 Jan 11
IBEX Orbit # 110 Perigee Contacts were nominal for command/telemetry and doppler data
The SSR and the FC was dumped along with 40 Blocks remaining from Orbit# 106
Date
Wednesday, January 26, 2011
Jday Time Station Controller CAR1 CAR2 CAR3 Razor# USNPR# Radius Earth S-Band Rate
026 0600 USHI01 SWesley 437 438 7 desc 320ksps
VC 0 VC 0 Seq Err VC 1 VC 1 Seq Err VC 2 VC 2 Seq Err PASS/FAIL
1130 0 17279 0 Pass
VC 2 Write Pointer Start 31322 VC 2 Write Pointer End 31383
VC 2 Read Pointer Start 14085 VC 2 Read Pointer End 31324
Orbit# 110 SSR_Dump/Tracking Contact
Blind_Acq.scr(320ksps)
CAR# 437 Re-Dump Orbit# 106 SSR_Blocks 1.(start 85070, 20 blks) 2.(start 85510,20 blks)
CAR# 438 Upload Orbit# 112 ATS (3-11 Feb 11) 1.IBEX_2011_034_00_00_v002.scr(302-369)
reset-master_timer.scr
SSR_Dump.scr(new)
@ECT_SetRelay stx,off $TIME=2011/01:26:06:37:00 (370)
ops_set_sc_time.scr
@0600 ebno=10.35 - 10.85 dbm (320ksps)
@0634 ebno=11.87 - 12.10 dbm (320ksps)
Date
Wednesday, January 26, 2011
Jday Time Station Controller CAR1 CAR2 CAR3 Razor# USNPR# Radius Earth S-Band Rate
026 1900 USHI01 SWesley 15 asc 64ksps
VC 0 VC 0 Seq Err VC 1 VC 1 Seq Err VC 2 VC 2 Seq Err PASS/FAIL
776 28 1033 286 Pass
VC 2 Write Pointer Start 32294 VC 2 Write Pointer End 32457
VC 2 Read Pointer Start 31324 VC 2 Read Pointer End 31324
Orbit# 110 Tracking Contact
@FTG_DumpBackOrbit (from statrt,0,0,0,0)
@FMI_SetDownlink(160ksps)
@1859 ebno=8.38 - 9.94 dbm (64ksps)
@1922 ebno=7.90 - 9.63 dbm (64ksps)
@1923 ebno=4.04 - 6.06 dbm (160ksps)
@1936 ebno=4.00 - 5.78 dbm (160ksps)
IBEX 26 Jan 11 Target Vectors
J2000 Spin Axis
ECI X=0.595319
ECI Y=-0.741464
ECI Z=-0.309558
-0.35611400=ActNor.EstInrToBdy[0]
0.72661000=ActNor.EstInrToBdy[1]
-0.57329000=ActNor.EstInrToBdy[2]
0.12868400=ActNor.EstInrToBdy[3]
980104000.000=ActNor.EstTime
Precession Maneuver
MPS Diff=0.621 deg
*MPS Diff should be < 1.5*
IBEX Spin Zxis (+Z S/C)
Right Ascension - RA=308.761 deg
Declination - DEC=-18.033 deg
IBEX Spin Axis vs. Sun Vector
IBEX Sun Angle=0.629 deg
IBEX Orbit# 110 MPS Target Vectors
MPS Cmd Vector X=0.596941464
MPS Cmd Vector Y=-0.736186579
MPS Cmd Vector Z=-0.318889022
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