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MEIDEX Operational Philosophy

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Abundance is different throughout the year. ROIs are limited ... Worm Drive. Worm Gear. SEKAI Camera. Lower End Plate. Upper End Plate. w/ Quartz Window ... – PowerPoint PPT presentation

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Title: MEIDEX Operational Philosophy


1
MEIDEX Operational Philosophy
  • IAF
  • Space Branch
  • Major Meir Moalem

2
Problem
  • Dust storms are random events
  • So are sprites
  • Abundance is different throughout the year
  • ROIs are limited
  • Airplane location - another constraint

3
Solution
  • Define rigid ROIs
  • Have a valid forecast
  • Maximize observation opportunities
  • Record every pass of ROI with sufficient lighting
  • Additional degree of freedom (truss)
  • Allow for flexibility in operational activation
  • Collect a large sample of scientific data
  • Define secondary, tertiary missions

4
General
  • Aerosols backscattered light measurements
  • Xybion multi-spectral camera, 6 W/L NIR to NUV,
    1410 FOV
  • SEKAI CCD viewfinder, 60º FOV
  • ADVCR digital recorders, 360 min total time
  • Canister with 16" quartz window and HMDA
  • Operated by PGSC WIN98 software
  • Backup recording at the AFD (DSR-20)

5
The MEIDEX Payload
Upper support plates
Upper End Platew/ Quartz Window
Lens and Baffle
Gimbal Motor and Worm Drive
Optical Bench/Support
Bearing and Brake (both sides)
Worm Gear
Xybion Camera
SEKAI Camera
Avionics Mount Platew/ electronics
Lower End Plate
6
Operational Event Cycle
  • Dust forecast
  • Observation planning
  • Where (if exists) is the dust plume?
  • Where is the Shuttle?
  • Where is the airplane?
  • Secondary mission?
  • Execute package
  • Observation
  • Astronaut (operations, backup, feedback)
  • Quick analysis and re-plan

Fusion
7
Whos Who and Where
  • TAU forecast center
  • POCC
  • Air Plane Base (Crete)
  • Aeronet stations
  • Sprites VLF stations

8
POCC Exp. Command Control
TAU forecast center
Med. ROI
Atlantic ROI
SPRITES
Global coordination in Real Time
STK scenario
9
Secondary Missions
  • Sprites ionospheric TLEs
  • Sea surface (Albedo)
  • Slant visibility studies

10
Nominal (aerosols) Operations
  • Bay-to-earth attitude, -ZLV directed to pass
    target (as forecasted), nadir view or a small
    bias
  • Activate payload, use SEKAI for orientation
  • fine tune truss pointing to dust plum (if
    possible)
  • Record science data on MEIDEX canister and AFD
    (DSR-20)
  • Monitor storm developments
  • Supply ground planners with any useful
    information

11
Sprite Operations
  • General convective forecasts, large possible
    areas (stk pic)
  • Earth limb view attitude
  • Tail (or nose) to earth
  • Bay away from RAM
  • FOV pointing above horizon
  • Record lightning activity
  • fine tune with truss

12
Execute Package
  • Whats in it?
  • Time of operations
  • Location of targets (dust plumes, sprites)
  • Location of airplane
  • Forecast maps
  • Payload related data \ instructions
  • Any other remarks
  • When will it be provided?
  • 24H in advance
  • 1-2 times per mission day / shift

13
Example Day 007
  • Data from mission timeline
  • 4 observational opportunities
  • 2 dust, 2 sprites
  • STK scenario
  • Where is the shuttle?
  • Where is the airplane?
  • Define exact timeline for operation
  • Ex. Pkg.
  • Observation from space, monitor from ground
  • Feedback? Changes between orbits

14
Back-up Recording
  • Recording within the payload 360 min.
  • Backup 1 DSR-20
  • First to start recording, last to stop
  • Used for playback to ground when no KU
  • Backup 2 digital VCR at JSC, records playback
    orbits
  • Backup 3 analog at GSFC
  • Degraded quality, probably not sufficient for
    scientific analysis

15
Calibration
  • Moon calibration
  • Shuttle moon pointing maneuver
  • Moon entering the Xybion FOV
  • Maintain a 2-5 deg. Deadband for 10 min.
  • Problem
  • Alignment of experiment with the -ZLV
  • Perform an alignment check on a pre-determined
    target

16
POCC Operations
  • When
  • A PS is not available
  • Target of opportunities
  • What is required
  • Open the HMDA (the door)
  • AFD recording
  • Real-time video downlink

17
Anomalies
  • Possible reasons
  • Failures (use redundancy, camera definitions)
  • Special scientific input (filter change)
  • Pre-defined from ground in the Ex. Pkg.
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