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LSST Alignment

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Final system is f/1.25: 51 m per arcsecond. Image error ... Precision limited by fiducial placement during fabrication. Final Alignment. What are the issues: ... – PowerPoint PPT presentation

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Title: LSST Alignment


1
LSST Alignment
  • C. F. Claver (NOAO)
  • J. H. Burge (UofA, Steward Obs.)

2
Outline
  • LSST Imaging requirements
  • Specific Concerns
  • Initial Alignment Concept
  • Final Alignment Simulation
  • Maintaining Alignment
  • Summary

3
Specific Concerns
  • Fast optics demanding image quality
  • Primary is f/1
  • Final system is f/1.25 51?m per arcsecond
  • Image error budget is tight
  • 0.5? site 0.33? total system ? 0.6? delivered
  • LSST optics 0.12?
  • Remaining error budget 0.30?
  • Complex system, many degrees of freedom

4
Initial Alignment
  • Precision Metrology
  • Fabrication
  • Surface-Substrate
  • Substrate-Fiducials
  • Assembly
  • Optical fiducials to structure
  • Commercial Solutions
  • Differential
  • 0.06 resolution
  • 9µm 2µm/m accuracy
  • 3µm 1µm/m repeatability
  • Absolute
  • 20µm 1.1µm/m accuracy
  • 7µm 1µm/m repeatability
  • Range
  • 35m

5
Initial Alignment Concept
  • Optics within view of laser ranging
  • Two locations
  • Redundant measurement
  • M1
  • Instrument
  • Precision limited by fiducial placement during
    fabrication

6
Final Alignment
  • What are the issues
  • Can the wavefront be sensed well enough to
    converge on system specs?
  • How field many positions?
  • What signal-to-noise?
  • Is there a unique solution?
  • Do we care?

7
Simulation Process
Initializemodel
500 models
Perturb degrees of freedom
Record initial merit function
Measure wavefronts
Add noise
5 times
Solve for best imagery
Record solved merit function
8
Degrees of Freedom
  • Rigid Body
  • 5 DoF for each
  • Primary M1
  • Secondary M2
  • Tertiary M3
  • Surface Deformation
  • M1 12 modes
  • M2 6 modes
  • M3 6 modes

39 degrees of freedom
9
Tolerances
  • Rigid Body
  • M1
  • Translation ?0.5mm in each of 3 axes
  • Tilt ?60? about 2 axes ? to optical axis
  • M2 M3
  • Translation ?0.25mm in each of 3 axes
  • Tilit ?60? about 2 axes ? to optical axis
  • Surface Deformation
  • M1
  • Z4-Z9 ?3.25?m (?5 waves _at_650nm)
  • Z10-Z15 ?1.30?m (?2 waves)
  • M2 M3
  • Z4-Z9 ?1.30?m (?2 waves)

10
Wavefront Measurement
  • 60 measured quantities
  • 5 Field Positions
  • Zernike Terms Z4-Z15
  • In Situ Curvature Sensing
  • Ad-hoc noise model
  • 0.05?m minimum uncertainty
  • 20 of Zernike term in quadrature

11
Simulated Curvature Sensing
  • Perturbed Optical model
  • Before and after extra-focal images
  • EF wavefront solution
  • Compare against Zemax wavefront error

12
EF vs Zemax Wavefront
  • Good agreement between calculated Zemax wavefront
    and recovered wavefront.
  • Recovered wavefront falls mostly within error
    envelope.

13
Solve for the degees of freedom
  • Using Zemax
  • Each DoF becomes a variable
  • Optimize model using noisy wavefronts as targets
  • Evaluate differences between solution and
    unperturbed model
  • Correct perturbed model using calculated
    differences
  • Record weighted spot size merit function

14
Initial Perturbed State
  • Merit Function
  • 9 field positions
  • weighted by effective area
  • 500 Models
  • Mean 118 ?m
  • STDEV 39 ?m
  • Max 245 ?m
  • Min 22 ?m

15
Monte Carlo Results
  • Put stats here

16
Merit Function Final Distribution
  • 91.2 lt 10?m after 5 iterations
  • All models once below 10 ?m, stay!

17
Remaining Issues
  • Maintaining Alignment
  • At what frequency are measurements required
  • How often to update solutions
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