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Segment Alignment Maintenance System

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HET SAMS Objective. HET is a spectroscopic survey ... SAMS is intended to be an edge sensor system on the HET to maintain the primary ... SAMS Program ... – PowerPoint PPT presentation

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Title: Segment Alignment Maintenance System


1
Segment Alignment Maintenance System for
the Hobby-Eberly Telescope
John Rakoczy NASA MSFC
2
HET SAMS Objective
  • HET is a spectroscopic survey telescope built by
    McDonald Observatory.
  • HET has an effective 9-meter aperture seeking
    seeing-limited performance.
  • SAMS is intended to be an edge sensor system on
    the HET to maintain the primary mirror figure in
    the presence of thermoelastic disturbances to the
    HET.

3
SAMS Program
  • MSFC is prime contractor under Space Act
    Agreement and Memorandum of Understanding with
    the University of Texas at Austin. MSFC manages
    system integration and verification.
  • Blue Line Engineering of Colorado Springs,
    Colorado is subcontractor. Blue Line provides
    inductive edge sensors and processing
    electronics.

4
Hobby-Eberly Telescope Primary Mirror
11.0 meters
Sub Array Test Cluster
5
Sub Array Test Sensor Layout
30
25
24
19
15
88
10
x denotes active coil o denotes passive coil
6
Basic Sensor Design
7
(No Transcript)
8
Edge Sensors mounted at intersection of 3
segments
Local Segment Electronics Node
9
Stackable System Processor
10
MSFCs Key Responsibilities
  • Control System architecture definition and
    algorithm development
  • System software development
  • FEM analysis and experimental validation of
    mirror mass loading requirements
  • System integration and testing

11
Program Milestones Accomplished
  • Completed Edge Sensor Proof-of-Concept Test
  • Completed Preliminary Design Review
  • Completed Sub Array Test on 7-segment subarray of
    HET
  • Completed Critical Design Review

12
Sub Array Test Quantitative Results Achieved
  • RMS Tip/Tilt errors lt 0.08 arcseconds
  • RMS Piston errors lt 2 microns
  • Global Radius of Curvature (GRoC) maintained lt
    300 microns
  • Edge Sensors provide better than 50 nm accuracy
    RMS
  • Sensor head mass lt 50 grams
  • Reliable continuous operation gt 10 days
  • Seeing limited image on 14th magnitude star

13
On-sky Image 5-April 0200
M20 EE50 1.15 arcseconds
Reference Stack
SAMS Stack EE50 1.57 arcseconds
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