The “Cobra” Fiber Positioner, the WFMOS Design, and Potential lessons for DESpec Michael Seiffert, Jet Propulsion Laboratory Richard Ellis, Caltech DESpec.

Slides:



Advertisements
Similar presentations
University College London, Optical Science Laboratory bHROS Progress bench-mounted High Resolution Optical Spectrograph bHROS bHROS Progress General.
Advertisements

Optical Lumped Element MKIDs Ben Mazin, February 2012 The Optical/UV MKID Team: UCSB: Ben Mazin, Sean McHugh, Kieran O’Brien, Seth Meeker, Erik Langman,
CMSC 2006 Orlando Active Alignment System for the LSST William J. Gressler LSST Project National Optical Astronomy Observatory (NOAO) Scott Sandwith New.
DESpec spectrographs Jennifer Marshall Darren DePoy Texas A&M University.
Spectroscopic Reference Design Options D. L. DePoy Texas A&M University.
Range Imaging and Pose Estimation of Non-Cooperative Targets using Structured Light Dr Frank Pipitone, Head, Sensor Based Systems Group Navy Center for.
Géraldine Guerri Post-doc CSL
Mohawk A proposed fiber positioner for MS-DESI Will Saunders, Greg Smith, Jamie Gilbert, Lew Waller, Tony Farrell, Gabriella Frost, Andy Sheinis, Peter.
 Michael J. Sholl 1, Mark R. Ackerman 2, Chris Bebek 3, Robert Besuner 1, Arjun Dey 4, Jerry Edelstein 1, Patrick Jelinsky 1, Michael L. Lampton 1, Michael.
Pore Detection in Small Diameter Bores The University of Michigan, Ann Arbor NSF Engineering Research Center for Reconfigurable Manufacturing Systems.
LBT AGW units Design Review Mar.2001 General Concept Performance specifications and goals The off-axis unit The mechanical support structure The control.
Fiber Repositioning System NanoDrop December 11, 2006 Chris Czech Charles Dielmann Mark Howe Dana Kimpton Christopher Sherman.
Optical Alignment with Computer Generated Holograms
M2FS: Michigan/Magellan Fiber System. M2FS (Michigan/Magellan Fiber System) Fiber-fed MOS w/2 independent and identical spectrograph arms 256 total fibers.
An Echidna-style positioner for DESpec
NGAO Alignment Plan See KAON 719 P. Wizinowich. 2 Introduction KAON 719 is intended to define & describe the alignments that will need to be performed.
WBS & AO Controls Jason Chin, Don Gavel, Erik Johansson, Mark Reinig Design Meeting (Team meeting #10) Sept 17 th, 2007.
Atacama Large Millimeter/submillimeter Array Expanded Very Large Array Robert C. Byrd Green Bank Telescope Very Long Baseline Array Green Bank Laser Rangefinders.
PLATO kick-off meeting 09-Nov-2010 PLATO Payload overall architecture.
1 DESpec Outline Concept Technical Components –Optics –Fiber Positioner –Fibers & Spectrographs –CCD & RO Some discussion about choices that may be available.
Generation-X telescope: Measurement of On-Orbit Adjustment Data Dan Schwartz, R. J. Brissenden, M. Elvis, G. Fabbiano, T. Gaetz, D. Jerius, M. Juda, P.
EDGE™ Final Project Plan P09701 – Corning Tropel LightGage™ Metrology System Matthew Bradley (ME) Images Courtesy of Corning Tropel.
An Echidna-style positioner for DESpec Will Saunders 8 March 2011.
A U.S. Department of Energy Office of Science Laboratory Operated by The University of Chicago Argonne National Laboratory Office of Science U.S. Department.
Ch 25 1 Chapter 25 Optical Instruments © 2006, B.J. Lieb Some figures electronically reproduced by permission of Pearson Education, Inc., Upper Saddle.
Figuring large off-axis segments to the diffraction limit Hubert Martin Steward Observatory University of Arizona.
Lab 3 - Centering. Centering; or the smart way to align centered optical elements and systems This lab will make use of concepts used in the previous.
Oct 17, 2001SALT PFIS PDR - Structure1 Structure Interface/ constraints Loads Structure design rationale Truss Weight and CG Finite Element Analysis/ Image.

Eddington Kick-Off. Vienna, September 17th, 2001 T.Muñoz/C.Laviada (INTA) 1 EddiCam: The Eddington Photometric Camera Preliminary Design Layout.
SAM PDR1 SAM LGS Mechanical Design A. Montane, A. Tokovinin, H. Ochoa SAM LGS Preliminary Design Review September 2007, La Serena.
Prime Focus Option (Ming Liang) Actuator Intro/Overview/Status Prime focus slides from M. Liang (NOAO) M. Sholl University of California at Berkeley Space.
The major advantages of USMs are: 1. Compact, lightweight, flexible and robust. 2. High positioning accuracy. 3. High low-speed torque and holding.
Peter Gillingham, Stan Miziarski, and Urs Klauser (Anglo-Australian Observatory) Figure 1 View of OzPoz showing the front of the focal late in observig.
HESSI Imaging Capability Pre Environmental Review Brian R. Dennis GSFC Tuesday, February 29, 2000.
FMOS Overview Oxford, 22nd June FMOS: Fibre Multi-Object Spectrograph Logical successor to 2dF Logical successor to 2dF Wide-Field IR spectroscopy.
Oct 17, 2001SALT PFIS Preliminary Design Review Optical Integration and Test Plan 1 Southern African Large Telescope Prime Focus Imaging Spectrograph Optical.
High Resolution Echelle Spectrograph for Chinese Weihai 1m Telescope. Leiwang, Yongtian Zhu, Zhongwen Hu Nanjing institute of Astronomical Optics Technology.
Understanding typical users for this instrument Graduate studentGraduate student –not an X-ray expert but wants to make a spatially resolved measurement;
6/11/2012 Building on NEAT concept - M. Gai - INAF-OATo 1 Building on NEAT concept M. Gai – INAF-OATo (a) Extension of science case (b) Payload implementation.
February 2013 Ground Layer Adaptive Optics (GLAO) Experiment on Mauna Kea Doug Toomey.
PFI Cobra/MC simulator Peter Mao. purpose develop algorithms for fiducial (FF) and science (SF) fiber identification under representative operating conditions.
3.1 Optomechanical systems (1) Scientific and engineering resources are available to carry out the optomechanical work on DECam. The highly distributed.
SAM PDR1 S OAR Adaptive Module LGS LGSsystem Andrei Tokovinin SAM LGS Preliminary Design Review September 2007, La Serena.
January 25, 2005GRETINA 2004 Review1 GRETINA 2004 Annual Review Steve Virostek Lawrence Berkeley National Lab Mechanical System.
The FMOS Facility for the SUBARU telescope Gavin Dalton Oxford/RAL.
Zero field The 25 ‑ m f /0.7 primary mirror for the Giant Magellan Telescope (GMT) is made of seven 8.4 ‑ m segments in a close packed array. Each of the.
A global approach to ELT instrument developments J.-G. Cuby for the French ELT WG.
3.1.1 Optics, Optical Corrector, Mechanical Systems M. Johns, C. Claver.
Henry Heetderks Space Sciences Laboratory, UCB
FELT 1 Study of the capability and configuration of a fixed mirror Extremely Large Telescope (FELT) Low cost path to large telescope Primary concern is.
POSITIONER SPECIFICATIONS 2250 fibres (c.f. ~400 for FMOS-Echidna) Field diameter ~320mm (c.f. ~150mm for FMOS-Echidna) Fibre core diameter 60µm Spherical.
Oct 17, 2001SALT PFIS Preliminary Design Review1 Southern African Large Telescope Prime Focus Imaging Spectrograph Mechanical Mechanism Design Michael.
Binospec - Next Generation Optical Spectrograph for the MMT
MECHATRONICS Lecture 05 Slovak University of Technology Faculty of Material Science and Technology in Trnava.
Mechanical design meeting, IAG, Calibration Unit mechanical design Svend M. Bauer Andreas Kelz, Emil Popow, Martin M. Roth.
1 System Architecture Mark Herring (Stephen Merkowitz Presenting)
IFS prototype – PM3 LAM, 13/06/2003 Prototype testing at CRAL Tests at room temperature in the visible.
Astronomical Observational Techniques and Instrumentation
N A S A G O D D A R D S P A C E F L I G H T C E N T E R I n s t r u m e n t S y n t h e s i s a n d A n a l y s i s L a b o r a t o r y APS Formation Sensor.
Upgrade PO M. Tyndel, MIWG Review plans p1 Nov 1 st, CERN Module integration Review – Decision process  Information will be gathered for each concept.
High power fibered optical components for gravitational waves detector Matthieu Gosselin, PhD Student at EGO ELiTES : 3 rd general meeting February 10.
Outline Sample preparation Instrument setting Data acquisition Imaging software Spring 2009AFM Lab.
CASE spectrograph Spectrograph Optical Specifications
Lab 3 - Centering.
Internal CDR meeting December 20th, 2005
Dr. Zainal salam; Power Electronics and Drives (Version 2),2002, UTMJB
MultiView 400™ Product Presentation Nanonics MultiView 400™
LightGage™ Frequency Scanning Technology
Breakout Session SC3 – Undulator
Presentation transcript:

The “Cobra” Fiber Positioner, the WFMOS Design, and Potential lessons for DESpec Michael Seiffert, Jet Propulsion Laboratory Richard Ellis, Caltech DESpec RAS and University College London March 2011 p.1

p.2 Density: Should roughly match desired target density. Practically, this means ~ 1000 sources/deg 2 At 4-8m telescope prime focus with typical plate scale this translates to positioner separation of ~ 10mm. Number: many 1000s. Maximize subject to budget constraint. Throughput Efficiency: Positioning accuracy should be high, and losses due to tilt, despace, and non-telecentricity should be small. Reconfiguration Speed: Fiber movement and position verification should proceed rapidly compared to exposure time. Robustness: A mechanically stiff system facilitates accuracy and allows lenses at fiber tip or other treatment of fiber ends. Fiber Positioner Design Considerations

Prime Focus Unit includes Wide Field Corrector (WFC) and Fiber Positioner. Spectrograph located above Naysmith platform Fiber connector mounted on top end structure Fiber Cable routed around elevation axis and brings light to the Spectrographs 3 WFMOS Concepts Are Relevant to DESpec Although the detailed designs are different, WFMOS, PFS and DESpec may share system aspects

Prime Focus Instrument (PFI) 4 In the WFMOS and PFS designs, several Subaru provided elements (field rotator, hexapod and wide field corrector) are shared with the HyperSuprimeCam

Rotator Interface Ring Positioner Equipment Bench Cobra Optic Bench Alignment System Cobra Modules with Drive Electronics 2400 Cobra Fiber Positioners 5 Rotating Portion of PFI

Positioner Optical Bench with 2400 Positioner Units 1 Positioner Unit - Cobra 6 Room for >4000 positioners 8mm apart in hexagonal pattern to enable field tiling

Positioner Element – “Cobra” Each motor rotates to provide complete coverage of the patrol region. Optical fibers mounted in “fiber arm” which attaches to upper postioner axis: Fiber runs through the center of the positioner – this couples the positioner and fiber system schedules and work efforts First axis of rotation Second axis of rotation Patrol Region Top View Fiber Tip Cobra 7 Theta stage Phi stage Fiber arm

8mm Cobra Positioner Patrol Area (9.5 mm dia.) Theta Stage (2.4 mm radius) Phi Stage (2.4 mm radius) Geometry 8

Patrol Region – Area of the focal plane accessible to one fiber (9.5 mm diameter) Patrol Regions Patrol Region may have zero or may have many potential astronomical targets Allocation efficiency describes the success rate in assigning targets to fibers Adjacent patrol regions overlap with no gaps 9 Low target densities: degree of overlap between patrol regions is unimportant. Important not to have gaps. High target densities: degree of overlap not important – there are many targets in each patrol region to choose from Intermediate target densities: (target density ~ positioner density) there is some benefit to having larger overlap.

Positioner Electronics Boards Positioner Module A module is a subassembly of actuators and drive electronics boards – Staggered production – Parallel module integration – Early mechanical and electrical functional testing – Parallel fiber integration to reduce schedule – Increases serviceability 10

Motors Commercially available rotating tube motor: High torque when stationary and unpowered ~ 1 mN-m powered torque 1 mrad resolution 1 – 10 rev/sec speed – Pairs of PZT plates oscillate in tandem bending – Drive signals of the two PZT plates are phase shifted by 90 degrees – This creates a traveling wave on the stator that excites the rotor like a harmonic gearbox to rotate the shaft by extremely small angles

Cobra Prototype 1 st stage motor 2 nd stage motor Fiber optic Ceramic friction drive Lubrication free, zero backlash Journal bearing limits motor side loads Hardstops to limit fiber twisting 5 um precision of fiber positioning Motor movement < 1 sec/iteration 12 Cobra system tested at JPL in partnership with New Scale Technologies Achieves 5μm positioning accuracy in 6 iterations Prototype has also successfully completed lifetime and environmental testing.

13 Prototype array of positioners is an essential precursor to proposing for a ~ element system Proposed laboratory and on-sky testing of 19-element system via NSF/Caltech $ Cobra fiber positioners Proposed 7-element prototype to demonstrate mechanical integration, tolerances, & integrated electronics fiducial fibers Multiplexed motor electronics

Metrology Camera – establishes science fiber positions relative to fixed fiducial fibers on positioner focal plane WFMOS concept: Four camera systems each looking at a ¼ of the focal plane. Located on prime focus support struts looking back at positioner focal plane via primary. Each camera is 4k by 4k CCD with 15μm pixels. Cameras are defocused to allow centroiding. Future: Larger format (10 k x 10k) single camera? Are back-illuminated CCDs (better centroiding) really required? Metrology camera (1 of 4 shown) 14

Back-lit fiducial fibers used to establish position of science fibers on positioner plane. Encoder fibers used to establish rotation orientation Science fibers are back-lit in a sequence to allow discrimination between fibers in the overlap regions between adjacent fibers, 1/3 at at time. In one exposure only the fibers marked (1) are illuminated, the next exposure only the ones marked (2) are illuminated, etc  Positioner moves elements in 3 groups of 800  Metrology camera views back-illuminated fibers. Fibers are illuminated in 3 groups of 800.  Movement, illumination, camera readout, computation in parallel  6 iterations can be completed in < 40 seconds

Fiber connector options APOGEE: US Conec 30 fiber connectors “ganging” with custom fixture allowing simultaneous mating of 300 fibers. Wilson et al., 2010 WFMOS team B study: Custom connector for 800 fibers with simultaneous mating. De Oliveira,

Key challenge of fiber-fed spectrographs: getting the fiber placed accurately on the astronomical target – large field of view – large number of fibers – smaller diameter fiber Make sure the system design addresses these challenges: – Robust positioner design provides high precision – attention to differential mechanical flexure in overall structure – error budgets for mechanical tolerances – Correction for non-telecentricity? – Include imaging mode with fast readout for verification! 17

WFMOS design emphasizes instrument efficiency: stiff, robust, & precise positioner system with fast reconfiguration speed Lifetime, thermal, and simulated altitude testing of prototype complete. Dust or other contamination testing TBD. Now engaged in the PFS design effort Two proposals now pending for small array demonstration. Critical to demonstrate that technical risks are retired and costs are understood before scaling up to thousands of elements. – Internal JPL proposal pending for 7 element lab module – NSF proposal pending for 19 element, on-sky, Palomar demonstration Investigation now underway of improved fiber coupling. Concepts include elimination of fiber twist, tilt of fiber end for non-telecentricty correction, and inclusion of small lens at the fiber tip for f-ratio conversion. 18 Conclusions & Future directions