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PCS Pointing Control Subsystem

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... between the PCS 'predicted' versus the GCS 'measured' guide star location ... OK for GCS to verify the guide star is positioned on the hotspot before ... – PowerPoint PPT presentation

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Title: PCS Pointing Control Subsystem


1
LBT Q3 2008 Eng/SW Review
  • PCS Pointing Control Subsystem
  • Michele De La Peña

2
Highlights
  • PCS Interfaces (GCS, MCSPU)
  • GCS Pointing Correction
  • Improved algorithm which applies the difference
    between the PCS predicted versus the GCS
    measured guide star location
  • Better handshaking implemented to indicate when
    it is OK for GCS to verify the guide star is
    positioned on the hotspot before closing the
    guide loop
  • MCSPU PCS Cold Start and New Target Trajectories
  • Better handshaking implemented which alleviates
    having to issue duplicate Presets - Late PCS
    trajectory communication ? mount/rotator enters
    HOLD mode ? reduces observing efficiency
  • The philosophy is the mount should react to the
    ever-changing pointing demand - PCS is a pure
    compute engine while MCSPU has the responsibility
    to recognize discontinuities due to new target
    requests
  • Functionality to Support Instruments
  • New functionality allows the observer to
    reposition where a target is imaged in the
    instrument focal plane (hotspot update)
    pointing origin update vs dither.
  • Observers can update the effective target
    wavelength (due to changing filters) and not
    have to issue a new Preset ? improved efficiency

3
Open Issues
  • Technical
  • Investigation of guiding issues
    (jumps/jiggles/jitters)
  • Resolve the LBC guide correction growth problem
    ? random occurrence
  • Tuning of gains and filters used to modulate the
    Az/El guiding corrections to avoid
    over-correction and system oscillation
  • Discussion on-going and an actual plan being
    formulated for near-term data collection
  • Thorough examination of kernel guide correction
    filter and application
  • Resolve high elevation guide oscillations
    (somewhat addressed in new kernel)
  • Achieve definitive understanding of the various
    kernel angles, transformations, and trajectory
    offsets to apply a comprehensive solution for
    each instrument
  • Evaluate and utilize the updated (and slightly
    incompatible) pointing kernel
  • Schedule
  • Concern not enough on-sky testing time for
    technical observing
  • Primarily weather, but also sky time scarce
    resource for testing (unit and integration)
  • Reconcile expectations when programmer
    participating in on-sky instrument support and
    required to implement new and robust
    functionality
  • Financial
  • Continued support for RAL consulting
  • Resource
  • None

4
Planning (Q4/2008)
  • Resolution of the Open Issues (Oct)
  • Initiation of a new PCS GUI (Dec)
  • Incorporates the functionality from current PCS
    and Preset GUIs
  • Provides additional control and monitoring
  • Sets the migration path for binocular support
  • Implement telemetry module
  • True Binocular Support (Dec)
  • Implementation of basic structural modifications
    to PCS to accommodate the binocular arbitrator
    (Dec)
  • Define/design interface between the PCS and PSF
    for the tip/tilt computation (Q1/2009)
  • Elaborate/design the model for co-aligned and
    misaligned observations (Q1/2009)
  • Implementation commencement LBC emphasis
    (Q1/2009)
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