NAOMI
Commissioning Procedures at the WHT wht-naomi-33
DRAFT (Version date: 25th May 2000)
1.0
Introduction.
The commissioning process will be also be a
learning process and thus the test descriptions offer some options and
flexibility. Minor modifications to the procedures are acceptable if made to
improve efficiency and/or system performance without changing the test
objective. All procedural modifications should be documented. Weather and
schedule constraints may lead to the omission of some tests, e.g. recalibration
checks. Any omissions shall be approved by the ING.
The following list is not intended to be fully inclusive. Its purpose is to draw attention to areas that require particular attention. Experience has shown that the failure to satisfy some conditions listed can create significant problems for adaptive-optics systems.
1.
GHRIL bench
vibration checked.
2.
GHRIL bench
surface aligned to optical axis; axis height 150.0+ 0.5 mm.
3.
Telescope optics
and derotator in a clean condition.
4.
Seal installed
around derotator.
5.
Derotator axis
and pupil stability (< 0.036 pupil diameter) determined to be
satisfactory.
6.
Nasmyth focus
location defined at GHRIL.
7.
GHRIL electronics
room cooling system operational.
8.
Telescope
altitude and azimuth drives functioning satisfactorily without oscillations or
“jumps”.
3.0
Before Commissioning: Integration to the WHT, baseline calibration and
performance confirmation.
Code |
Objective(s) |
Requirements |
Description of Test |
Date &Examiner |
Pass/ Fail |
Comments |
1 |
Perform initial installation and alignment
of NAOMI and INGRID. |
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1.1 Installation and Alignment of the OMC1. The attached appendix gives the procedure for the optical alignment of the Opto-Mechanical Chassis (OMC). This must be completed successfully before the Nasmyth Calibration Unit (NCU) and then the wavefront sensor (WFS) are brought into alignment with it. 1.2 Installation and
Alignment of the NCU
2. 1.Install the NCU shelf on to the GHRIL bench. 3. Place the Nasmyth Calibration Unit (NCU) on the bench and shelf with the ball of the alignment aid (ATC drawing number 10a22a) in the chassis plate pivot hole. 4. Install the NFP mask at the Nasmyth focus. 5. Remove the Integrating Sphere Unit (ISU) if installed and replace with the f/11 alignment laser. 6. Turn on the f/11 laser.* 7. Ensure that f/11 NCU pupil mask is installed. 8. Install cross hairs on OAP1 (FSM) coincident with the optical axis. Check the centration with the MAT. 9. Adjust NCU jacking feet to bring the laser focus to the height of the central (on-axis) pinhole in the NFP mask. 10. Using the two grub screws on the alignment aid adjust the ball position until the pinhole is illuminated by the laser. Note that as the alignment proceeds the ball can be adjusted as required to keep the laser focus on axis. 11. Adjust the eccentric to bring the NCU optic axis (as defined by centre of laser beam relative to target cross hairs) into the x,z plane of the OMC. 12. Adjust the NCU feet into the x,z-plane of the OMC. 13. Iterate steps 10 to 13 if required until the NCU is aligned. 14. Lock the ball and remove alignment target. 1.3 Installation and
Alignment of the WFS 1. Install WFS on the bench in its nominal position using the approved handling procedure and make all connections. 2. Set WFS probe to the centre of its range in x, y and z and close WFS shutter. 3. Turn on f/11 He-Ne laser and verify that the beam is centred on the WFS pick-off mirrors and collimating lens. If not adjust the WFS centration and rotation as required. Turn off He-Ne laser. 4. Select WFS full-aperture doublet. 5. Select predetermined filters and set ADC to zero. 6. Turn on NCU white light source, WFS CCDs and insert NCU beamsplitter. 7. Manually install NFP mask. 8. Set WFS carriages to predetermined locations to view pinhole image. 9. Adjust WFS pick-off focus (z-axis) to give best focus of pinhole image. If motion is > 1mm readjust WFS position manually to bring refocusing within 1 mm[MW1]. 10. Select pupil fiducial in WFS. 11. Move CCD carriage to view pupil fiducial and image of dummy-DM mask. Rotate WFS manually about pivot point to centre mask image in x-axis on the fiducial. Rotate WFS first pick-off fold mirror if required to centre in y axis. Observe CCD display during this operation. 12. View NCU on-axis point source image with CCD and recentre/refocus if required by moving WFS probe in x,y or z directions.* 13. Iterate to obtain correct pupil and image position simultaneously. 14. Turn off NCU white light source. |
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2 |
Perform initial calibration and functional
checkout of OMC, WFS and NCU. |
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2.1 WFS Dark CountsThis simple procedure determines the number of dark counts, i.e. bias, for each pixel in the WFS CCDs. The variation with temperature and time will be explored. Note that the read noise may also be derived from this procedure. Assuming that the values are found stable and repeatable at all operational temperatures, dark-count correction will be performed with look-up tables. 1. Close WFS shutter. 2. Turn on WFS CCDs. 3. Record CCD dark counts over various intervals (TBD during system integration). 4. Record WFS temperature sensor readings. 5. Repeat at least hourly and over widest possible temperature range (as governed by GHRIL conditions) until bias variations can be reliably established. 6. Generate look-up tables to account for bias as a function of integration time and temperature. 7. Shutdown system power or reset to normal operation setup, as required. 2.2 WFS Flat FieldIn this procedure
the WFS calibration source is used to flat field the WFS CCDs but the NCU
on-axis point source could also be used for this purpose. 1.
Turn on WFS
power, WFS calibration source and control system. 2.
Select
predetermined WFS spectral and ND filters. 3.
Set WFS ADC to
zero deviation. 4.
Select lenslet
1 in lenslet wheel. 5.
Set WFS camera
focus position for lenslet 1 focus. 6.
Move WFS probe
to acquire WFS calibration source. 7.
Verify Hartmann
spot positions are satisfactory; if not adjust probe position. 8.
Select clear
aperture in lenslet wheel. 9.
Move camera
focus to view clear aperture. 10.
Record CCD
pixel intensities over a pre-determined integration period. 11.
Shutdown system power or reset to
normal operation setup, as required. 2.3 WFS internal collimationThis procedure
serves as a check that the light leaving the WFS collimating lens is properly
collimated and that the WFS carriage positions repeat from those established
in Durham. . If the light is not collimated the Hartmann spot spacing will
increase or decrease as one moves to the edges of the Hartmann spot array as
seen by the CCDs. The spot pattern will appear to exhibit either pincushion
or barrel distortion depending on whether the beam is divergent or
convergent. If a problem exists the distance between WFS pick-off and the collimating lens must be adjusted
until a uniform spot spacing is obtained. The reconstructor should, of
course, be used to provide a quantitative measure of defocus. 1.
Turn on WFS
power, WFS calibration source and control system. 2.
Select
predetermined WFS spectral and ND filters. 3.
Set WFS ADC to
zero deviation. 4.
Select lenslet
1 in lenslet wheel. 5.
Set WFS camera
focus position for lenslet 1 focus. 6.
Move WFS probe
to acquire WFS calibration source using x,y and z co-ordinates established in
Durham. 7.
Verify Hartmann
spot separations are uniform and determine defocus using the
reconstructor. If not adjust spacing
between pick-off and collimating lens until defocus is zero within the limits
set by system noise, i.e. change fore-optics focus position. Note that the
camera focus must also be adjusted to follow this focus change. 8.
Shutdown system power or reset to
normal operation setup, as required. 2.4 WFS transfer curve with WFS calibration sourceThis procedure
describes the procedure for generating a WFS transfer curve for a selected
lenslet array and CCD pixel binning configuration using the WFS calibration
source. By moving the WFS probe relative to the WFS calibration source in the
x-y plane one produces a tilt of the input wavefront. From the Hartmann spot
shifts and the focal length of the lenslet one can determine the measured
tilt (or phase gradient). A plot of the commanded tilt vs measured tilt
(ordinate axis) gives the transfer curve. The procedure may also be employed
in an iterative manner to set the WFS camera focus as described in the next
section. 1.
Turn on WFS
power, WFS calibration source and control system. 2.
Select
predetermined WFS spectral and ND filters. 3.
Set WFS ADC to
zero deviation. 4.
Select
specified lenslet in lenslet wheel. 5.
Select
specified WFS CCD camera pixel binning configuration. 6.
Set WFS camera
focus position to pre-determined (look up) focus. 7.
Move WFS probe
to acquire WFS calibration source. 8.
Move WFS probe
in pre-determined increments along x-axis and record spot positions for each
incremental step. 9.
Generate
transfer curve using measured spot positions for each incremental step. 10.
Repeat steps 7
and 8 but for y axis if desired. 11.
Shutdown system power or select the
next lenslet array and/or binning configuration as required. 2.5 WFS camera focus This procedure is
used to check the focus of a selected lenslet array. As the CCD relay lens
relay lens is telecentric the effect of a focus change is a change in spot
size but without a centroid shift. Uniform illumination of the each lenslet
is assumed for this statement to hold true. Probably the best measure of
focus is to determine the slope of the WFS transfer curve, i.e. the steepest slope is given at best focus.
Thus the procedure is functionally the same as that given in the preceding
section.. 1.
Turn on WFS
power, WFS calibration source and control system. 2.
Select
predetermined WFS spectral and ND filters. 3.
Set WFS ADC to
zero deviation. 4.
Select
specified lenslet in lenslet wheel. 5.
Select
specified WFS CCD camera binning conifiguration. 6.
Set WFS camera
focus position to pre-determined (look up) focus. 7.
Move WFS probe
to acquire WFS calibration source. 8.
Move WFS probe
in pre-determined increments along x-axis and record spot positions for each
incremental step. 9.
Generate
transfer curve using measured spot positions for each incremental step. 10.
Compare transfer
curve with previously determined curve in look-up table. 11.
If curve
differs from look-up table, i.e. smaller slope, change camera focus in
pre-determined incremental steps and repeat steps 7 and 8 for each focus
change until the maximum slope is obtained. 12.
Shutdown system power, select
another lenslet array or binning configuration or reset to normal operation
setup, as required. 2.6 WFS transfer curve using FSMThis procedure takes
into account the effect of the OMC aberrations on the WFS transfer curve.
Here the FSM is used to change the tilt of the input wavefront to the WFS.
The input wavefront is produced by the NCU on-axis point source. The
procedure could be performed for off-axis points if the NFP mask is
installed. Note that the NCU tip-tilt injection mirror could also be used in
place of the FSM if desired. 1.
Turn on power
to WFS, FSM, DM, NCU white light source and control system. 2.
Insert NCU
beamsplitter and ISU mask. 3.
Select
predetermined WFS/NCU spectral and ND
filters. 4.
Set WFS ADC to
zero deviation. 5.
Select
specified lenslet in lenslet wheel. 6.
Select
specified WFS CCD camera pixel binning configuration. 7.
Set DM stage
position in x and y from look-up table. 8.
Set WFS camera
focus position to pre-determined (look-up) focus. 9.
Flatten DM. 10.
Set FSM to
servo zero position (open loop). 11.
Move WFS probe
to acquire NCU point source using pre-determined coordinates and close
WFS_WFS pick-off loop to centre source in WFS field. 12.
Open loop and
verify Hartmann spot locations are satisfactory; if not readjust WFS probe
position. 13.
Incrementally
change FSM azimuth (x-axis) angle over a pre-determined range and record
Hartmann spot positions for each incremental change in tilt. 14.
Generate
transfer curve using measured spot positions for each incremental step. 15.
Repeat steps 11
and 12 for FSM elevation motion and/or diagonal motions if desired. 16.
Remove NCU
beamsplitter and ISU mask. 17. Shutdown system power, repeat procedure for another lenslet array or binning configuration or reset to normal operation setup, as required. 18. Note that, if desired, this procedure may also be performed using the ”turbulence-broadened” NCU source. 2.7 FSM to WFS loop checkThis procedure uses
the tip/tilt injection capability of the NCU to check the performance of the
FSM in closed loop operation when driven by tip/tilt error signals from the
WFS. 1.
Power up the
system. 2.
Turn on NCU
white light source. 3.
Insert the NCU
beamsplitter and the ISU mask. 4.
Flatten DM. 5.
Set FSM to
servo zero. 6.
Select
specified WFS lenslet array. 7.
Select
specified WFS camera pixel binning configuration. 8.
Set WFS ADC to
zero deviation. 9.
Set DM stage to
required x-y position from look-up table. 10.
Set WFS probe
to pre-determined co-ordinates to acquire NCU on-axis point source. 11.
Optimise WFS
probe position if required. 12.
View source
with acquisition camera. 13.
Install camera
or position sensor (TBD) on axis at optical science port (OSP) to view NCU
point source. 14.
Set NCU
tip/tilt injection mirror to pre-determined amplitude and frequency. 15.
Confirm
frequency and amplitude of point source using acquisition camera (if former
is within camera bandwidth). 16.
Close FSM-WFS
loop. 17.
Observe/record
residual spot jitter as seen by OSP camera/sensor. Compare to previous
results obtained during integration. 18.
Turn off NCU
white light source. 19.
Remove NCU
beamsplitter and ISU mask. 20.
Shutdown system power or reset to
normal operation setup, as required 2.8 Nasmyth focal plane to WFS probe spaceHere the Nasmyth
focal plane (NFP) mask with its array of pinholes is used to calibrate the
WFS probe space. 1.
Manually
install the NFP mask at the Nasmyth focal plane. 2
Turn on power
to WFS, FSM, DM, NCU white light source and control system. 3
Insert NCU
beamsplitter. 4
Select
predetermined WFS/NCU spectral and ND
filters. 5
Set WFS ADC to
zero deviation. 6
Select
specified WFS camera pixel binning configuration. 7
Select full
aperture doublet in lenslet wheel. 8
Set WFS camera
focus position to pre-determined (look up) focus. 9
Flatten DM. 10
Set FSM to
servo zero position (open loop). 11
Move WFS probe
in x and y to acquire each NFP point source in turn. Centre each point source
image in the camera and record the WFS probe coordinates. 12
Generate
look-up table of NFP position vs. WFS probe position. 13
Remove NFP
mask. 14
Remove NCU
beamsplitter and turn off the NCU white light source. 15
Shutdown system
power or reset to normal operation setup, as required. |
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3 |
Repeat acceptance tests performed at Durham
to verify that system performance has not degraded. |
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1.
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4 |
Measure non-common-path offsets between WFS
and INGRID using the NCU as a reference source. |
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1.
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First Light: Preliminary
Commissioning Tests
Code |
Objective(s) |
Requirements |
Description of Test |
Date &Examiner |
Pass/ Fail |
Comments |
5 |
Demonstrate the satisfactory completion of
the set-up procedures in preparation for observation of a science object. |
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5.1 Initialise WFSThis procedure uses only an artificial star to initialise the WFS and thus it does not determine the effect of the WHT aberrations. The effects of differential aberrations between the on-axis and off-axis images, for example, may be handled by look-up tables. One may find that this procedure best serves as a check on the repeatability and stability of NAOMI. This will perform the following operations: 1. Power up the system. 2. Insert NCU beamsplitter , predetermined NCU filters and ISU mask. 3. Set WFS probe to on-axis position. 4. Set WFS filters to predetermined values. 5. Set WFS ADCs to zero dispersion. 6. Select predetermined lenslet array. 7. Select specified WFS camera pixel binning configuration. 8. Set DM stage positions in x and y from look-up table. 9. Turn on NCU white light source. 10. Set Science Camera to snapshot mode. 11. Flatten deformable mirror and zero tip-tilt mirror. 12. Determine Hartmann spot centroids on WFS 13. Close loop on on-axis point source. 14. With feed-back from Science camera determine optimum centroid offsets and pistons 15. Repeat step 14 for other lenslet arrays. 16. Open loop. 17. Display information on WFS set-up, if acceptable proceed. 18. Switch off NCU white light source. 19. Remove NCU beam-splitter. 20. Shutdown power or reset to normal operational setup. 5.2 TCS CalibrateThere are two possible approaches to this calibration. The first is to use the acquisition camera. This approach is preferred for its simplicity. Current estimates from the ING predict a camera sensitivity of 18th visual magnitude after initial commissioning tests. This sensitivity should be more than adequate for a standard TCS calibration. The second approach is to use the WFS to determine the relative positions of the artificial (from the NCU) and natural guide stars. This approach should offer somewhat higher accuracy if required. Note that both approaches have been successfully used during MARTINI runs. As a calibration accuracy of around 1 arcsecond is acceptable for most observing scenarios there is usually no requirement for a compensated NGS image. The first approach involves the following operations: 1. Turn on power to NCU, acquisition camera and associated display and electronics. 2. Insert NCU beam-splitter and ISU mask 3. Select predetermined NCU spectral and ND filters 4. Turn on NCU on-axis white light source 5. Display point-source image (artificial star) in acquisition camera field 6. Determine and record image position taking into account any allowance for the beamsplitter offset 7. Turn-off NCU white light source and remove ISU mask 8. Command TCS to selected natural star (reference star) 9. Determine and record time-averaged natural star position 10. Repeat steps 7 and 8 as needed for other reference stars 11. Remove NCU beam-splitter and ISU mask The second approach involves the following operations: 1. Turn on NAOMI power 2. Put in NCU beam-splitter 3. Select WFS doublet, predetermined filters and zero WFS pick-off offsets 4. Flatten DM 5. FSM to zero 6. Turn on NCU on-axis artificial star 7. Acquire with WFS and centre in its field by closing WFS_WFS pick-off loop 8. Turn off artificial star and open WFS_WFS pick-off loop 9. Command TCS to selected natural reference star 10. Verify acquisition with acquisition camera and record position in acquisition field. 11. Remove NCU beamsplitter 12. Acquire reference star and centre in WFS field by adjusting TCS pointing. 13. Verify star centration in WFS by time-averaging its position; adjust TCS pointing if required. 14. Insert NCU beamsplitter and determine new star position in acquisition camera field. 15. Difference between initial and final TCS gives TCS correction required. 16. Repeat steps 9 to 15 for other reference stars if required 5.3 Acquire Set-up StarHere we acquire and observe a corrected image of a suitable bright star within a few arcseconds of the science object of interest. The star will be used to check the AO system closed-loop performance, check the focus of the INGRID and determine the seeing parameters. The assumption is made that the system power is already on. Acquisition involves the following operations: 1. Select suitable bright star 2. Select WFS specified lenslet array 3. Set DM and FSM loops open 4. Flatten DM 5. Set FSM to zero 6. Turn on the acquisition camera and insert NCU beamsplitter 7. Set all colour and ND filters to predetermined values 8. Centre star within acquisition camera field 9. Move telescope to required field such that light from bright star passes into the WFS (drag and drop operation) then remove NCU beamsplitter. 10. Set DM position in x and y from look-up table 11. Set WFS ADC to PA 12. Further adjustment of telescope might be required to align star perfectly. 13. Close DM and FSM loops with low gain 5.4 Set TCS FocusAn iterative approach is suggested. The primary operation here is to set the WHT secondary mirror position to provide the optimum focus at the science instrument (INGRID during initial operation). One must also ensure that for this condition the WFS focus is such that the focus offload to the secondary is zero. 1. Set TCS focus to predetermined value (believed to best focus for INGRID) 2. Check uncorrected science image of suitable bright star and correct if obvious defocus 3. Close loop following steps 3 to 13 in section 4.3 above 4. Change WFS focus so that offload to TCS is zero. 5. Time average several science frames and inspect PSF 6. Change WHT secondary focus by distance TBD 7. Change WFS focus so that offload to TCS is zero. 8. Time average several science frames and inspect PSF 9. Compare PSF to previous PSF 10. Repeat steps 6, 7, 8 and 9 as appropriate until PSF indicates best focus has been obtained 5.5 Determine Seeing ParametersWith open-loop operation on bright star the following seeing parameters will be determined: 1. Determine r0, t0 from WFS data 2. Determine optimum lenslet array size and focal length (set by guide star brightness and turbulence conditions – may be a look-up table) 3. Determine optimum conjugate height (upgrade only – method TBD) 4. Query astronomer if suggested lenslet array (and conjugate choice – upgrade) acceptable, if so continue, if not enter own choice. 5. Set lenslet array 6. Set conjugate lens (upgrade only) If lenslet array or conjugate lens changed redo WFS initialisation. 5.6 Determine Sky Background For WFSThis procedure determines the level of sky background that will be seen by the WFS during the observations. The assumption is made that this procedure immediately follows the determination of seeing parameters, i.e. one can point the telescope such that the WFS sees the sky background in the region of the science object(s) and the astronomer knows the WFS operating parameters to be used while observing. 1. Move WFS probe to appropriate region of sky. 2. Select pre-determined WFS lenslet array, filters and WFS camera operating mode. 3. Record WFS signals over integration period and number of frames TBD. |
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6 |
Implement the observational procedure and
establish WFS response using star(s) of known magnitude and spectral
characteristics. |
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Here a typical
observational procedure is followed
using various stars to establish the
WFS response. Suitable stars shall be selected prior to commissioning. 6.1 Set up target (guide star) parametersThe following observing options must be set; these can either be set before the run and stored in a data file or interactively set for a new target. 1. Co-ordinates of science target 2. desired field position of science object 3. Set Sky PA 4. WFS guide star offsets + spectral type and magnitude if available 5. WFS Colour/ND Filters 6. Wide/Narrow field correction required (depending on science field of interest) 7. Sky chopping offsets and direction 8. Continuous optimisation during exposure on/off 6.2 Acquire targetThis will perform the following: 1. Open all mirror loops 2. Move telescope to required field (start slew) - this is a command to place the guide star onto the WFS probe position 3. Set sky PA 4. Insert NCU beamsplitter 5. Verify guide star location in acquisition camera field 6. Move WFS probe to guide star location 7. Remove NCU beamsplitter 8. Flatten DM and zero FSM servo 9. Set DM stage to x and y positions from look-up table 10. Select specified lenslet array (determined in section 4.5) 11. Set WFS offsets and filters 12. Set WFS ADC 13. Display WFS acquisition display and verify target in field 6.3 Align science target/guide starTwo displays will be available. 1. Science camera field. 2. Display of the WFS image and signals. On the acquisition display a target star might be positioned on the WFS pick-off by moving the telescope. This might perhaps be done by clicking on the star and dragging it to sensor pick-off position or by moving the pick-off by clicking on the sensor pick-off box and dragging it onto the star. A possible alignment procedure might proceed as follows: 1. Close WFS-FSM loop {select lenslets} and commence TCS offload . Engage tilt bandwidth optimisation. CHECK: photon levels against expectation and system limits. 2. If astronomical object is visible on the science camera use this to move it to the desired field position if required. This move will be performed by executing a probe offset procedure with the FSM loop closed (at least before and after). The displays and user interface must provide a mechanism for determining and executing this offset. 6.4 Determine closed-loop parametersThis will perform the following operations: 1. Close DM loop 2.
Initiate automatic control loop
optimisation 3. Show astronomer selected optimised parameters and performance metrics (oscilloscope display). Astronomer can enter own parameters if desired. 6.5 Science camera exposure (if desired for information purposes)Exposures may now be taken. At end of exposure the following information to image header file: 1. Observing options which were selected 2. r0, t0 estimate 3. Guide star count rate 4. RMS residuals on wavefront 5. Tag to file containing further seeing/performance parameters
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7 |
Establish closed loop limit for “current”
seeing, i.e. determine limiting stellar magnitude at which a satisfactory
loop closure can be achieved. |
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This test may be
regarded as an extension of the previous test (Procedures 6.1 to 6.5). Loop
closure (6.4) is attempted with successively fainter stars (TBD) until a
satisfactory closure cannot be obtained.
The limit variation
as a function of star spectral class and integration time should be explored
subject to schedule constraints and weather conditions. |
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8 |
Determine maximum
no-oscillation bandwidth and gains with “current” seeing using a bright star.
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1.
A bright guide
star is acquired and observed closed loop following the observational
procedures 6.1 to 6.5. 2.
The WFS
integration time is progressively reduced to allow operation at higher
bandwidths. The effect of gain variations are explored as part of this
process. |
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Advanced Characterisation
Code |
Objective(s) |
Requirements |
Description of Test |
Date &Examiner |
Pass/ Fail |
Comments |
9 |
Determine the effect
of binary objects as a WFS reference on system performance. |
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10 |
Assess system
stability |
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11 |
Evaluate schemes for
measuring off-axis WFS offsets for optimum IR imaging. |
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Two options are
proposed. Selection of the best method will be made during commissioning. The
selection process will be driven by the linearity and stability of the DM and
WFS offsets. From the viewpoint of simplicity the first procedure is currently regarded as the default. Use of DM to measure differential
aberrations between science object and guide star
1.
Power up the
system. 2.
Set PA using
TCS to place guide star at location within the science field where science
object will be placed. FSM and DM loops are open (FSM at servo zero and DM
flattened). 3.
Select
specified WFS lenslet array and camera pixel binning configuration. 4.
Set WFS AtDC
for PA. 5.
Set DM stage
position in x and y from look-up table. 6.
Position WFS
probe to acquire guide star and close WFS-WFS pick-off offset loop. (Note:
This loop automatically centres the WFS probe on the guide star and it is not
be confused with offsets of the Hartmann spots. The latter are referred to as
the WFS offsets.) 7.
Close FSM and
DM loops. 8.
Optimise IR
image (method TBD) and record time-averaged WFS and/or DM offsets. 9.
Position the
guide star at its operating position and re-acquire with the WFS as in step
6. 10.
Close FSM loop. 11.
Differential
WFS offsets are determined by either: keeping the DM
offsets at the values determined in step 8 and noting the time-averaged
change in WFS offsets or servoing the WFS
offsets to be the same as those determined in step 8 and noting the change in
the time-averaged DM offsets. 12. Shutdown power or reset to normal operating configuration. Use of an NCU
diffraction limited on-axis source
1.
Power up the
system. 2.
Manually
install the NFP mask. 3.
Select
predetermined WFS/NCU spectral and ND filters. 4.
Turn on NCU
white light source and insert NCU beamsplitter. 5.
Select
specified WFS lenslet array and camera pixel binning configuration. 6.
Set WFS AtDC to
zero deviation. 7.
Set DM stage
position in x and y using look-up table. 8.
Flatten DM and
zero FSM servo. 9.
Move WFS in x
and y to centre on each pinhole source within FOV covered by the science
camera. Use method (TBD) to optimise each IR image and determine the DM
and/or WFS offsets. 10.
Remove NFP
mask, turn off NCU source and remove beamsplitter.. 11.
Produce map of
differential aberrations between on-axis and off-axis images 12.
Acquire an
on-axis guide star (see Section___) and measure time-averaged WFS offsets. 13.
Insert NCU
beamsplitter and repeat step 11. Offload focus error introduced by
beamsplitter to TCS. Note that the
differential WFS offsets between steps 12 and 13 give the aberrations
(>defocus) introduced by the beamsplitter. Note also that the chromatic
shift between visible and K-band should be negligible but should be checked
during commissioning. 14.
Insert ISU mask
and turn on NCU white light source to give diffraction-limited K-band and
visible sources on axis. 15.
Use TCS to move
guide star approximately 10 arcseconds off axis with WFS centred on the NCU
on-axis visible point source. 16.
Optimise image
of NCU K-band source in science camera. Record the DM and/or WFS offsets. 17.
Use TCS to
place guide star at position to be used during observations. 18.
Move WFS to
acquire guide star. 19.
Optimise IR
image of on-axis NCU source. Note science object may be used instead for this
optimisation if it is bright enough. Record the DM and/or WFS offsets. 20.
Record the
differential offsets between steps 15 and 18; these data provide the off-axis
telescope aberrations. 21.
Remove NCU
beamsplitter and ISU mask. Turn off the NCU white light source. All differential
offsets can then be used to calculate the operational WFS offsets with guide
star and science object as shown in Figure 1a. Off-axis offsets
For NAOMI + camera from data in step 12.
For telescope from data in steps 16 and 19.
Beamsplitter offsets
Offsets due to the insertion of the NCU beamsplitter are given by data from steps 12 and 13. |
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Demonstrate the
ability to maintain loop closure during dithering. (Requirement?) |
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