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Page 1: Prototyping the GMT Telescope Metrology System …...measuring each primary mirror with respect to the corresponding corrector. Test hardware, develop software. Integrate with the

Presented by

Prototyping the GMT Telescope Metrology System on LBT

Andrew RakichOptical Designer

Page 2: Prototyping the GMT Telescope Metrology System …...measuring each primary mirror with respect to the corresponding corrector. Test hardware, develop software. Integrate with the

Summary

Description of Laser Truss Metrology System

Etalon Absolute Multiline Technology

Prototyping on LBT

Results to date

Future work

Page 3: Prototyping the GMT Telescope Metrology System …...measuring each primary mirror with respect to the corresponding corrector. Test hardware, develop software. Integrate with the

In 2016 GMTO adopted the idea of a “Telescope Metrology System” (TMS) into the baseline plan.

▪ Seen to address a gap between the expected accuracy of open-loop modelling of optics positions given thermal and gravity deflections, and “good” starting points for the Acquisition, Guiding and Wavefront Sensing system (AGWS).

▪ The system allows the measurement and control of all mirror segments, aligning them to the Gregorian Rotator axis, with errors at the micron level, and with measurement cadences of several seconds.

▪ Of several 3-D metrology technological approaches considered, a “Laser Truss” incorporating multiple fixed absolute-distance-measuring interferometers, was selected.

▪ Given that this technology had never been employed on ground based telescopes, it was deemed necessary to conduct an extensive prototyping and R&D program prior to finalizing the GMT design.

The GMT Telescope Metrology System

Andrew Rakich Prototyping the GMT Telescope Metrology System on LBT 3

Page 4: Prototyping the GMT Telescope Metrology System …...measuring each primary mirror with respect to the corresponding corrector. Test hardware, develop software. Integrate with the

A commercial absolute distance measuring interferometer system was selected for the laser truss.

▪ Up to 800 independent metrology channels.

▪ Measurement uncertainty (in air) 0.5 µm/m

▪ Maximum measurement frequency > 500 kHz (can be used as vibrometer with much higher accuracy for high frequencies)

▪ Measurement length > 30 m

▪ Simple measurement channel consisting only of telecom fiber, collimator and triple reflector (no electrical systems on telescope)

▪ Almost unlimited fiber length possible (several kilometers)

▪ Eye safe infrared radiation

▪ Metrological traceability by gas absorption cell

▪ All componentry based on “industry hardened” high I/O telecom equipment.

Etalon Absolute Metrology Technology (EAMT)

Andrew Rakich Prototyping the GMT Telescope Metrology System on LBT 4

Page 5: Prototyping the GMT Telescope Metrology System …...measuring each primary mirror with respect to the corresponding corrector. Test hardware, develop software. Integrate with the

In 2017 GMTO proposed to prototype the metrology system on LBT.

▪ Gives LBTO the opportunity to trial new metrology technology without large capital expenditure.

▪ Opportunity for GMTO to gain first-hand and long-term experience with Laser Truss metrology on a working telescope.

▪ LBT 22.5 m optical baseline and 8.4 m diameter borosilicate mirrors give the closest match to GMT of any working large telescope today.

▪ Conveniently located, not so far from Pasadena, and with a common partner institution in Steward Observatory.

▪ GMTO technical staff already very familiar with LBTO active optics systems.

▪ A 3-phased prototyping effort began in August 2017.

Prototyping on LBT

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Page 6: Prototyping the GMT Telescope Metrology System …...measuring each primary mirror with respect to the corresponding corrector. Test hardware, develop software. Integrate with the

The prototyping effort is divided into three phases:

▪ Phase 1: Deploy laser truss on the prime focus cameras, measuring each primary mirror with respect to the corresponding corrector. Test hardware, develop software. Integrate with the Telescope Control System (TCS).

▪ Phase 2: Deploy Laser Truss for the Gregorian Telescope. Measure M1, M2 and M3 relative to an instrument rotator. Integrate with TCS.

▪ Phase 3: Control both Gregorian Telescopes and measure between right and left telescopes for interferometric baseline control.

▪ At this stage Phase 1 is basically complete and hardware is en-route for phase 2.

Prototyping Phases

Andrew Rakich Prototyping the GMT Telescope Metrology System on LBT 6

Page 7: Prototyping the GMT Telescope Metrology System …...measuring each primary mirror with respect to the corresponding corrector. Test hardware, develop software. Integrate with the

Phase 1 results

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Page 8: Prototyping the GMT Telescope Metrology System …...measuring each primary mirror with respect to the corresponding corrector. Test hardware, develop software. Integrate with the

Closed dome measurements: Swing Arm Repeatability

Andrew Rakich Prototyping the GMT Telescope Metrology System on LBT 8

-35

-30

-25

-20

-15

-10

-5

0

5

10

15

0 5 10 15 20 25 30

LBC R Swing Arm Repeatibility

Retro 1: del X Retro 1: Del Y Retro 1: Del Z Retro 2: Del X Retro 2: Del Y

Retro 2: Del Z Retro 3: Del X Retro 3: Del Y Retro 3: Del Z

Page 9: Prototyping the GMT Telescope Metrology System …...measuring each primary mirror with respect to the corresponding corrector. Test hardware, develop software. Integrate with the

Closed dome measurements: Thermal Drift

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Page 10: Prototyping the GMT Telescope Metrology System …...measuring each primary mirror with respect to the corresponding corrector. Test hardware, develop software. Integrate with the

Closed dome measurements: Elevation

Andrew Rakich Prototyping the GMT Telescope Metrology System on LBT 10

-0.5

-0.4

-0.3

-0.2

-0.1

0

0.1

0 20 40 60 80 100 120 140 160 180

X and Y deflections in millimeters

-120

-100

-80

-60

-40

-20

0

20

02

:09:4

3

02

:10:1

8

02

:10:5

4

02

:11:3

3

02

:12:0

9

02

:12:4

4

02

:13:2

0

02

:13:5

5

02

:14:3

1

02

:15:0

7

02

:15:4

2

02

:16:1

7

02

:16:5

3

02

:17:2

8

02

:18:0

5

02

:18:4

1

02

:19:1

7

02

:19:5

4

02

:20:3

1

02

:21:0

7

02

:21:4

3

02

:22:2

0

02

:22:5

6

02

:23:3

2

02

:24:0

9

02

:24:4

6

02

:25:2

2

02

:25:5

9

02

:26:3

5

02

:27:1

2

02

:27:4

8

02

:28:2

4

02

:29:0

5

02

:29:4

1

02

:30:1

7

02

:30:5

4

02

:31:3

0

02

:32:0

6

02

:32:4

3

02

:33:1

9

02

:33:5

6

02

:34:3

2

02

:35:0

9

02

:35:4

4

02

:36:2

1

02

:36:5

7

02

:37:3

4

02

:38:0

9

deltas in Rx and Ry (arcseconds)

delta Rx delta Ry

Page 11: Prototyping the GMT Telescope Metrology System …...measuring each primary mirror with respect to the corresponding corrector. Test hardware, develop software. Integrate with the

Closed dome measurements: Signal strength over the elevation range

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Page 12: Prototyping the GMT Telescope Metrology System …...measuring each primary mirror with respect to the corresponding corrector. Test hardware, develop software. Integrate with the

“Passive” Observing

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Page 13: Prototyping the GMT Telescope Metrology System …...measuring each primary mirror with respect to the corresponding corrector. Test hardware, develop software. Integrate with the

The EAMT system has its own software that fullycontrols the unit.

This software can be accessed by other programson the observatory network via a TCP/IP interface.All of the control, measurement and analysisfunctions of the native EAMT software can becalled by another program over TCP/IP.

For our prototyping effort a Python script has beenwritten that commands the EAMT to take ameasurement, requests the resultant data ondifferential motion of the target retroreflectors, anddoes the necessary mathematics to produce avector of M1 mirror position commands

𝑥, 𝑦, 𝑧, 𝑅𝑥 , 𝑅𝑦 , such that the mirror is returned to

the last “good” position relative to the corrector.

The Python script then hands this vector to a PERLscript that interfaces with the TCS.

Software

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Page 14: Prototyping the GMT Telescope Metrology System …...measuring each primary mirror with respect to the corresponding corrector. Test hardware, develop software. Integrate with the

The change in relative position of the mirror and corrector at a given TMS measurement can be decomposedinto “good” and “bad” changes. The good changes are the various commanded mirror position changes thathave been applied since the original TMS reference measurement was made.

These must to be taken into account before applying corrections to the mirror position. Essentially the“goalposts” move and this must be taken into account.

The PERL script interface to the TCS subtracts the following known offsets from the raw measurement andapplies the difference to a mirror position command.

- Pointing offsets

- Instrument offsets (filter focus, say).

- Active optics focus offsets.

- Active Optics M1 motions due to Z11 and Z22 (spherical aberration) corrections.

- Guiding offsets.

Software

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Page 15: Prototyping the GMT Telescope Metrology System …...measuring each primary mirror with respect to the corresponding corrector. Test hardware, develop software. Integrate with the

Very limited use of the system for full active control has so far been made, as the prime focus correctors are only in use ~ 10% of the time and further engineering time, which is heavily subscribed, is required to deliver a system ready for routine observing.

The following result shows the TMS maintaining alignment during a transiting exo-planet observation that tracked a defocused star through Zenith for 40 minutes.

There was no noticeable change in the PSF during the observation, a result that improved on a similar observation without the TMS.

Active Control

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Page 16: Prototyping the GMT Telescope Metrology System …...measuring each primary mirror with respect to the corresponding corrector. Test hardware, develop software. Integrate with the

When the variables of telescope and software conspired towork during our limited time in active control of the telescope,the results have been promising.

After collimating the telescope at a high elevation, and lockingoptics positions with the TMS, the telescope can be slewed tolow elevations with no noticeable misalignment of the optics.

With the latest modifications to the control software, furtherengineering time is required to qualify the system for routineuse during science operations.

Active Control

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Page 17: Prototyping the GMT Telescope Metrology System …...measuring each primary mirror with respect to the corresponding corrector. Test hardware, develop software. Integrate with the

▪ Hardware robust and reliable.

▪ TCP/IP communication and control works well.

▪ Collimator alignment maintenance is not an issue.

▪ 1” collimators give superior results to ½” collimators.

▪ Good signal maintained over collimation model range of LBT.

▪ There are no measurable stray light issues for science instruments utilizing CCD detectors.

▪ Achievable accuracies appear to be excellent and as expected.

▪ Range of temperature from +20C to -10C handled without problems from operability point of view.

▪ Temperature measurement in situ is important.

▪ System maintenance of relative position of main telescope optics to within several micron level errors seems to be a reasonable expectation.

Lessons learned to date.

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Page 18: Prototyping the GMT Telescope Metrology System …...measuring each primary mirror with respect to the corresponding corrector. Test hardware, develop software. Integrate with the

▪ Hardware has been purchased for the extension to Phase Two and Three prototyping: the control of the Gregorian Telescope.

▪ More quantitative performance information is expected from these phases because of the superior performance of the Shack Hartman Wavefront sensors in Gregorian modes.

▪ Gregorian metrology is expected to begin in September 2018.

▪ Further details of the systems performance such as for mirror radius measurement to sub micron levels and nanometric 3-D vibration trace measurement will be discussed in the paper.

▪ The prototyping effort to date has yielded valuable information that validates the technological approach to assisting in telescope alignment.

Future Work and conclusion.

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Page 19: Prototyping the GMT Telescope Metrology System …...measuring each primary mirror with respect to the corresponding corrector. Test hardware, develop software. Integrate with the

Development Team

GMTO:

Andrew Rakich, Patricio Schuter, Mathieu Bec, Rod Conan

LBTO:

John Hill, Mike Gairdner, Mathieu Bec, Olga Kuhn and the LBT Mountain crew

Etalon Ag.:

Heinrich Schwenke, Mark Wissmann, Kai Brenner, Yousef Rhanavard

Page 20: Prototyping the GMT Telescope Metrology System …...measuring each primary mirror with respect to the corresponding corrector. Test hardware, develop software. Integrate with the

Thanks

GMTO take this opportunity to thank LBTO and Etalon AG. For their support and collaboration in this prototyping effort.

Page 21: Prototyping the GMT Telescope Metrology System …...measuring each primary mirror with respect to the corresponding corrector. Test hardware, develop software. Integrate with the

Author/Presenter Name Presentation Title GMTO Corporation |21