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Mission Operations Status August 7, 2006

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Propellant Usage & Lifetime Estimates. Overall Summary. Additional Slides: ... No impact to operations or 6-year life expectancy. 13. Aqua Mission Operations Status ... – PowerPoint PPT presentation

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Title: Mission Operations Status August 7, 2006


1
Mission Operations Status August 7, 2006
EOS Aqua
  • Bill Guit
  • Aqua/Aura Mission Director - Code 581
  • phone 301-614-5188
  • fax 301-614-5267
  • William.J.Guit_at_nasa.gov

2
Topics
  • Spacecraft Performance Summary
  • Major Activities Completed (since Aug 05)
  • Planned Activities
  • Anomalies (since Aug 05)
  • Propellant Usage Lifetime Estimates
  • Overall Summary
  • Additional Slides
  • Maneuvers and Ground Track Error
  • Back-Up Anomaly Slides (BMA-2 Cell 4 SSR)
  • Back-Up Aqua Project EOL Disposal Options

3
Aqua Spacecraft Subsystems
  • Command Data Handling (CDH) Nominal
  • Solid State Recorder (SSR) holds 2 orbits of
    data
  • Minor SSR Performance Anomaly (April 10, 2006)
  • Communications (COMM) - Nominal
  • Electrical Power System (EPS) Nominal
  • ARE 4A continues to perform at lower level
  • Battery Cell Anomaly (September 2, 2005)
  • Flight Software (FSW) - Nominal
  • Guidance, Navigation Control (GNC) - Nominal
  • Propulsion (PROP) - Nominal
  • Thermal Control System (TCS) Nominal

All subsystems configured to primary hardware
4
Spacecraft Subsystem Status Summary
5
Major Activities Anomalies (Since Aug 2005)
  • Aug 23rd HQ Briefing
  • Sep 2nd Battery Cell 4 Anomaly
  • Dec 1st Drag Make-Up Maneuver (DMUM) 24
  • Waived off due to Orbital Debris concerns
  • Dec 31st Leap Second
  • Apr 14th Expanded Direct Broadcast
  • Apr 28th CloudSat (CS) CALIPSO (CP) Launched
  • May 27th 31st CS CP Orbit Raising Complete
  • May 4th 4-Year Anniversary
  • May 18th Loaded Special AIRS Stored Command
    Sequences (SCSs) for DMUM Waive Offs
  • Jun 7th Norway Communications Outage
  • Jul 5th Norway Communication Outage

6
Planned Activities
  • Inclination Adjust Maneuvers (IAMs)
  • August 22nd 29th
  • September 7th, 12th, 19th 26th
  • October 3rd (Back-Up Date)
  • Coordinated A-Train IAM Plan Developed
  • Sep 22nd EPS State-of-Health Test 5 (_at_Equinox)
  • Oct 20th Solar Eclipse 10
  • Dec 31st Leap Second (NONE Planned for 2006)
  • TBD HSB Turn-On Test 14
  • TBD EEPROM Refresh

7
Aqua Inclination Adjust
8
Inclination Adjust Maneuvers (Aug/Sep/Oct 2006)

9
Maneuver Locations
10
Long-Term Plans
  • Aqua/Aura Single-S/C-Ops
  • Goal is to operate Aqua and Aura as if they were
    a single spacecraft and reduce staff where
    feasible
  • Take advantage of spacecraft similarities
  • Aqua/Aura Auto Ops (Dump-N-Go)
  • Goal is to provide a capability to retrieve
    Science Data in the event of a major
    communication outage
  • Eliminates the need for ground commanding for
    normal SSR operations
  • Science Team concerns over data losses due to
    Auto Ops
  • Aqua/Aura Automation (Lights-Dim Ops)
  • Goal is one person staffing during off-shift
    operations with fire-watch approach to
    anomalies and data losses

11
Spacecraft Anomalies
12
Spacecraft Anomalies
  • Battery Anomaly September 2, 2005
  • BMA-2 Cell 4 temperature exceeded its 10o C
    yellow high limit and charge/discharge voltage
    profile was also anomalous
  • Charge/discharge cycle subsequently returned to
    normal
  • Successfully implemented recommended charge
    profile changes (also implemented on EOS Aura)
  • Final Closeout Report released in March 2006
  • Most likely cause a variable, intermittent,
    unpredictable short
  • Root cause of shorting cannot be conclusively
    determined
  • Open action items being followed by EPS Working
    Group
  • Destructive Physical Analysis (DPA) Report
    released May 1st
  • Results of the DPAs did not produce any new
    recommendations for the flight operations of the
    Aqua or Aura spacecraft
  • No impact to operations or 6-year life expectancy

13
Spacecraft Anomalies
  • Solid State Recorder (SSR) Anomaly April 10,
    2006
  • Noticeable increase in the single bit error (SBE)
    rate detected by the SSR Error Detection and
    Correction (EDAC) was observed
  • Previous increases had been correlated with solar
    activity
  • Occurs approximately every other orbit
  • Nominal 5-20 SBEs per dump jumped to 100-170 per
    dump
  • Not near EDAC threshold of 680 counts
  • No increase in double bit errors
  • Flight Operations Team (FOT) continues to monitor
    by performing more frequent diagnostic dumps
  • Sub-module 205 responsible for the increase
  • No impact to science data collection

14
Old Spacecraft Anomalies
  • SADA Potentiometer OPEN
  • Noise observed on both POTs First observed in
    2003
  • Anticipate Aqua FSW modification(s) will be
    required
  • Noise exceeded FM threshold 7 times on 10/10/04
  • FOT continues to monitor performance
  • No current impact to operations
  • ARE-4A Anomaly OPEN
  • First observed on 8/13/04, then again on 9/9/04
    and 10/8/04
  • FOT generated Anomaly Report in December 2004
  • Discussed at each Power Systems Review
  • FOT continues to monitor performance
  • No current impact to operations

15
Data Losses(Since August 2005)
  • October 18, 2005 1h 4m 57s of Hi-Rate Science
  • Combination of EDOS problem with multiple
    operator errors on the part of the FOT
  • Resulted in High Rate Science Data Losses
  • MODIS 291/094301 104758 (1h 4m 57s )
  • AIRS 291/094303 104759 (1h 4m 56s )
  • Operations teams (EDOS FOT) conducted a root
    cause and corrective action analysis
  • Improvements in communications between EDOS and
    the FOT and procedural changes have been
    implemented
  • Should prevent a reoccurrence

16
Data Losses(Continued)
  • November 8, 2005 3m 4s of Hi-Rate Science
  • FOT Data Loss due to failed ground station
    contact
  • MODIS 312/174503-174807
  • AIRS 312/174505-174809
  • November 8, 2005 17m 30s of Hi-Rate Science
  • During recovery from the failed ground station
    contact, the FOT misplaced a tic () mark in
    contingency PROC, which resulted in a significant
    delay in the execution. This Ops Error resulted
    in an additional 17 minutes and 30 seconds of
    Hi-Rate Science data loss
  • MODIS 312/185932-191700
  • AIRS 312/185933-191702

17
Data Losses(Continued)
  • March 28, 2006 11s of Hi-Rate Science
  • Ground station antenna problem caused loss of
    command and telemetry
  • Allowed Partition 9 (high-rate science) to
    overwrite data before the next playback
  • FOT jammed the Partition 9 Read Pointer on the
    next contact to minimize the data loss
  • Data Loss Times
  • MODIS 2006-087/162806 162817z
  • AIRS 2006-087/162808 162818z

18
Data Losses(Continued)
  • June 7, 2006 Norway Communications Outage
  • Service provider disrupted service on the
    redundant circuit while trouble-shooting a
    problem on the prime circuit
  • Instrument Science Data Losses (3h 39m 24s)
  • MODIS 158/034553 072515 GMT
  • AIRS 158/034554 072517 GMT
  • July 5, 2006 Norway Communications Outage
  • Router in New York down at unmanned site
  • Instrument Science Data Losses (6h 43m 26s)
  • MODIS 186/005628 072232 GMT
  • AIRS 186/005628 072232 GMT
  • MODIS 186/083823 085545 GMT
  • AIRS 186/083828 085545 GMT
  • All Previous Data Losses Totaled 5h 2m 58s

19
Aqua Data Capture(Thru June 30, 2006)
20
Instrument Anomalies(NO NEW ANOMALIES)
21
Old Instrument Anomalies
  • CERES-Fore (FM4) Short-wave Anomaly - March 2005
  • March 30th at 089/1842 GMT the Short-wave
    channel bridge balance electronics failed to
    update the bridge settings as the space lamp
    value fell outside the established window of
    50-200 counts
  • No impact to Ops Loss of Redundancy
  • AMSU A1-2 Noisy Bus Current Rise - May 2005
  • ART concluded that the observed increase in scan
    motor current was indicative of normal wear and
    didnt warrant further investigation at this time
    Review every 6-Months
  • Observed increase as expected in May 2006
  • MODIS SpectroRadiometric Calibration Assembly
    (SRCA) Lamp 3 Anomaly May 2005
  • Modification to Ops completed Fall 2005
  • Final Anomaly Closeout Report completed Dec 2005

22
Propellant Usage Lifetime Estimate
23
Propellant Usage
Orbit Raise Maneuvers
Orbit Inclination Maneuvers
Orbit Inclination Maneuver Tests
24
Lifetime Estimate
Worst case analysis for Aqua would indicate
minimum of 8-10 years of remaining life saving
125kg of fuel for EOM ESMO Flight Dynamics
analysis indicates Aqua has sufficient propellant
reserves to last until 2015
25
Lifetime Estimate
26
Long-Term Solar Flux Predicts
27
Summary
  • Spacecraft Status - GREEN
  • Instrument Status - GREEN
  • AMSR-E, AIRS, AMSU, CERES MODIS
  • Operations Nominal Producing Great Science
  • HSB Survival Mode since 2/5/2003
  • Data Capture/L0 Processing Status GREEN
  • SSR Data Capture to 07/31/2005 99.989391
  • SSR Data Capture to 06/30/2006 99.547602
  • SSR Data Capture to 07/31/2006 TBD
  • Data Latency Excellent
  • Ground Systems Performing well and are meeting
    and/or exceeding requirements
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