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PALM-3000 Instrument Architecture. Antonin Bouchez PALM-3000 Requirements Review November 12, 2007. Instrument Concept. Instrument Requirements Document: http://www.oir.caltech.edu/twiki_oir/bin/view.cgi/Palomar/Palm3000/SystemsEngineering. PALMAO components to be reused: - PowerPoint PPT Presentation
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PALM-3000
PALM-3000 Instrument Architecture
Antonin Bouchez
PALM-3000 Requirements Review
November 12, 2007
PALM-3000
2
Instrument Concept
Instrument Requirements Document:http://www.oir.caltech.edu/twiki_oir/bin/view.cgi/Palomar/Palm3000/SystemsEngineering
PALMAO components to be reused:• AO cart (used to transport the AO system)
• AO spit (used to support the AO system during lab work)• AO optical bench and Cassegrain interface support structure.• Relay optics: eg. Off-axis parabolas (OAP), fast steering mirror (FSM), fold mirrors.• 349-actuator Xinetics deformable mirror (DM349).• Low-Order Wavefront Sensor (LOWFS), as an interim tip/tilt/focus sensor.
Project phases:• Phase 0: Interim relay (current optics recoated, focus shifted).• Phase 1: Develop and deploy DM3368, HOWFS, wavefront processor, etc.• Phase 2: Develop and deploy IRTT, TWFS and related electronics and software.
PALM-3000
OAP1
OAP2
FSM
DM3368
DM349
FM2
FM3
FM1
3
Optical Layout (1)
AO Stimulus:• Simultaneous NGS and LGS stimuli.• X-Y translation of NGS stimulus to accommodate multiple instruments.
AO Relay:• A single off-axis parabola relay.• DM3368 at the pupil• DM3349 conjugate to <±1.5 km.
PALM-3000
4
Optical Layout (2)
Beam splitter AO Mode
#1 #2 #3 Comments
NGS-IR open 970 LP open
LGS-IR 30% 1100-1780 R 970 LP 589 NR
NGS-IR from LGS-IR 30% 1100-1780 R 970 LP open 30% loss in sensitivity in J and H.
NGS-V open 50% R or 650 LP open #2 choice depends on science band.
LGS-V 1000-1780 R 595 LP 589 NR No science at <595 nm.
NGS-V from LGS-V 1000-1780 R 595 LP open No science at <595 nm.
Wavefront sensor beam splitting •Large beamsplitters (6-8”) are fixed, only changed out with instruments.• Splitter #3 on actuated stage to switch between NGS and LGS modes.• Space constraints pose greatest chanllenge.
PALM-3000Beam Splitter Layout Schematic
IRTT
HOWFS
TWFS
ACQ
Science Instrument
#1
#2 #3
PALM-3000
6
Wavefront Sensors
High Order WFS (Phase 1)• NGS and LGS sensor, using CCD50 detector (128x128)• 8x8, 16x16, 32x32, 64x64 pupil sampling.• Adjustable field stop for spatial filtering.
Infrared Tip/Tilt WFS (Phase 2)• Wide-field imaging camera based on HAWAII2-RG.• Full-field acquisition and region-of-interest readout.• Single filter, J+H (1100-1780nm).
Low-Order WFS (Phase 1)• 3x3 Shack-Hartmann sensor using CCD39.
Truth WFS (Phase 2)• 2x2 Shack-Hartmann sensor using CCD39• Provides focus and back-up tip/tilt capability.
PALM-3000
7
Electronics
Cassegrain Cage• Controller rack• DM349 driver rack• DM3368 driver rack.• Active cooling!
Computer room• Wavefront Processor:
NVIDIA 8800 GPUs (17)Housed in 9 PCs
• Telemetry serverData room• Operator workstation
CA
M
I/F
SW
T
I/F
GP
U 2
GP
U 1
CPU
PC 1
Bur
st
Dat
a R
AM
SW
T
I/F
Dis
k A
rray
CPU
PC 8
CA
M
I/F
SW
T
I/F
DM
I/
F
LW
FP
CPU
PC 0
Switched
Network
……
D/A
Data Server
Eth
er-
Net
I/
F
Gigabit Ethernet
Data User 1
Data User n
……
PALM-3000
8
DM control algorithms
Solution: Implement both pathways for DM349 control.
PALM-3000
9
Operational Systems Software
• Provide low-level control of all AO system functions (servo loop state, motor positions, etc.)
• Provide displays of system status and performance (live display of servo loop state, WFS pixels, DM actuator positions, servo loop strip charts).
• High-level automations:• Guide star acquisition on all wavefront sensors
• Wavefront sensor background recording• Wavefront sensor to DM registration• Flexure and atmospheric refraction compensation• Phase-diversity measurement of the static aberrations
seen by the science instrument• Optimization of the LGS reconstructor using Palomar
MASS Cn2 data
PALM-3000
10
Laser Guidestar Facility
Planned Improvements• Relocate the Chicago Sum
Frequency Laser to the lower Coude lab.
• Potentially space of a second laser in the same lab.
• Improvements to LLT image quality are still required.
• Aircraft safety system automation based on Table Mountain Observatory system.
Lower Coude