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PALM-3000 Status. A.H. Bouchez, J.E. Roberts Project 1640 Las Vegas Summit 1/28/2010. PALM-3000 status. The big picture: We are integrating the new PALM-3000 components in the lab, while a few remaining subsystems are in detailed design. We are on track for a pre-ship review in early July.
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PALM-3000 Status A.H. Bouchez, J.E. Roberts Project 1640 Las Vegas Summit 1/28/2010
PALM-3000 status The big picture: We are integrating the new PALM-3000 components in the lab, while a few remaining subsystems are in detailed design. We are on track for a pre-ship review in early July. Talk Outline: • Status by subsystem • 3388-actuator DM testing results • Integration and testing in 2010 • Commissioning plans in 2011
DM3388 OAP1 TTM OAP2 DM241 FM1 Science Instrument Volume FM3 SSM2 FM2 FM4 SSM1 HOWFS & ACam Optical Bench • Detailed design of all optomechanics is complete • Currently verifying global flexure of bench with science instrument • Remaining design tasks: • Stimulus fold mirror • Enclosure • Cable routing • Cable interface boxes
High-Order Deformable Mirror • Received at Caltech on Dec. 4, 2009 • Spent Dec-Jan. testing performance with a Zygo interferometer In the lab at Caltech Prior to face sheet bonding (Xinetics Inc.)
HODM testing • Tested with a Zygo in I&T testbed • Plastic curtains enclose bench to allow humidity control with dessicant • Data • Unpowered and bias voltage measurements at 40-50% RH, 10-15% RH and 20-30% RH • Actuator influence functions • Actuator Linearity • Actuator Hysteresis • Actuator Creep • Reconstructor made from the influence functions was used to flatten the mirror • Other control tests include controlling to the low spatial frequency error instead of flat and maximizing the focus error to test the full mirror stroke
HODM Control Result Surface Surface • Mirror in normal mode (40V bias) Temp: 75F RH: 26% • Zernikes 1-30 were removed from the bias measurement and the residual wavefront was flattened using the HODM actuators. The result is on the left. • On the right is the same measurement less Zernikes 1-30. This is what we can expect to achieve when the LODM is correcting the low-spatial-frequency errors
HODM lessons • The HODM can be flattened to 10nm RMS • Simulations show that resulting wavefront will not limit contrast performance • The total stroke of the mirror is 1.06μm. • A few actuators along the bottom of the mirror have significantly lower stroke • With the LODM, the HODM will use 30% of its stroke to correct its own figure • We need to control the humidity around the HODM • Best figure between 20% and 30% RH • 40V bias rather than the nominal 50V bias gives more stroke and a better base figure at the expense of more non-linearity in the actuator gains
Humidity Results • Unpowered surface figure at different humidities shows the effect of humidity on the puckers • Ideal humidity is between 13% and 30% 45% RH 74deg 13% RH 70deg 30% RH 74deg
High Order Wavefront Sensor • Complete and ready for installation in lab testbed • Flexure testing ongoing. Initial results meet requirements (<0.2”/hr) • Two optics need to be replaced: Will replace and realign later in spring • Acquisition camera (not shown) needs to be aligned and tested Meets requirements (<0.05 binned pixels) See Baranec, Proc. SPIE 7015, 2008.
HOWFS Detail Microlens arrays imaged with a CMOS alignment camera Shack-Hartmann spots imaged with the CCD-50
Electronics Overview Legend: Fiber, high-speed switch, ethernet, AO bench cables Ethernet Pvt net Fiber Splitter User Workstation (Data Room) AO Bench Wavefront Processor (computer room) DM Racks (Cass cage pos. 2 & 3) Controller Racks (Cass cage pos. 4 & 5)
DM Electronics and Cabling • Lab configuration complete and in use (serial com. to DM drivers, 99 cables, air cooled) • Current design efforts: • High-speed DM command electronics design in progress • Operational DM cable design in progress (16 cables for HODM, 1 for LODM) • Driver electronics dissipate ~6 kW. Liquid cooling design still required
Wavefront Processor Computer • Wavefront Processor Computer clusters completed and deployed (JPL and Caltech) • Significant challenge has been hardware/software compatibility. Manufacturer of high-speed switch went out of business. • Have demonstrated full vector matrix multiplication using 64x64 subapertures at 1.24 kHz with current GPUs • If necessary, will upgrade to latest GPUs after pre-ship review to meet 2 kHz requirement
Software Deep into coding & verifying interfaces. Expect to begin using software environment in the lab in Feb. Major components % Complete • Publish/subscribe infrastructure 100% • Command parser 95% • Includes communications interfaces • Wavefront processor 30% • Device drivers (hardware interfaces) 75% • Telemetry system 50% • Automations 25% • Graphical user interface 20%
Servo Control • Flexible servo control scheme. • Detailed design of N=64 mode complete • Detailed design of other modes still in progress
Palomar Infrastructure Currently defining requirements. Major components: • Power at Cassegrain focus (& AO lab) • Coolant at Cassegrain focus (& AO lab) • Telescope balance adjustments • Power in computer room • Communications between Cass, Computer Room, AO lab, and Data Room
PALM-3000 Testbed Includes HODM, HOWFS, WFP computer, and 3 calibration/diagnostic sensors Will allow us to verify all electronic & software interfaces. HODM Zygo WFP computer CMOS HOWFS & ACAM HASO
Lab I&T Schedule Testbed activities Dec-Jan Verify performance of HODM Feb-Mar Verify performance of HOWFS Mar-Apr Test wavefront processor, software environment May-Jun Verify high-speed wavefront control performance Jul SPIE meeting, pre-ship review