18/13/2015alex delacroix ngao laser guide star mechanical pdr
TRANSCRIPT
104/19/23 Alex Delacroix
NGAOLaser Guide Star
Mechanical
PDR
204/19/23 Alex Delacroix
1) LGS Asterism Arrangements
2) LGS Fixed Asterisms
2.1) LGS, Lower Fixed Asterism, Design Overview
2.2) LGS Fixed Asterism Probe Arm Design
2.3) LGS Fixed Asterism Gimbal Design
2.4) LGS Fixed Asterism Camera Assembly Adjustment Design
2.5) LGS, Central Fixed Asterism, Design Overview
3) LGS Patrolling Asterisms
3.1) LGS, Patrolling Asterism, Design Overview
3.2) LGS, Patrolling Asterism, Pick Off Arm Design
3.2.1) LGS, Probe Assembly Optical Design
3.2.1.1) LGS, Probe Assembly Optical Path
3.2.1.2) Static Load on the Lever Motor
3.2.1.3) Static Load on the Crank Motor
3.2.1.4) Probe position accuracy
3.2.1.5) Probe position repeatability
NGAOLaser Guide Star
Mechanical
304/19/23 Alex Delacroix
3.2.2) LGS, Probe Assembly Mechanical Design
3.2.2.1) LGS, Probe Assembly Limit Switch Mechanical Design
3.2.2.2) LGS, Probe Tip Design
3.2.2.3) LGS, Probe Tip Deflection
3.2.2.4) LGS, Probe Tip Frequency Analysis
3.2.3) LGS, Patrolling Asterism, Lever Assembly Design
3.2.4) LGS, Patrolling Asterism, Crank Assembly Design
3.3) LGS, Patrolling Asterism, Camera Assembly Design
4) LGS, Structure Design Overview
4.1) LGS, Plate Structure Assembly
4.2) LGS, Beam Support Assembly
4.3) LGS, Legs Assembly
NGAOLaser Guide Star
Mechanical
404/19/23 Alex Delacroix
1) LGS Asterisms arrangementThe Lgs is composed of 3 patrolling asterisms and 4 fixed asterisms, equally spaced around the central Field of view.
Fixed Asterism, lateral upper
Fixed Asterism, lateral, lower, left Fixed Asterism, lateral, lower, right
Patrolling Asterism, upper, left Patrolling Asterism, upper, right
Patrolling Asterism, lower
Fixed Asterism, center
LGS arrangementCurrent Mass Estimate: 80 Kg
504/19/23 Alex Delacroix
2) LGS Fixed AsterismThe Lgs fixed asterism is composed of three lateral probes pointing toward the center of the science field within a diameter of 14.5mm (20”) (FR-2360) and one central Channel. Each Channels are installed thru a three point kinematic mount, shimmed as required.
Fixed Asterism arrangement
Fixed Asterism Field of View
Fixed Asterism, lateral, upper
Fixed Asterism, lateral, lower, left
Fixed Asterism, lateral, lower, right
Fixed Asterism, center
Kinematic mount
Current Mass Estimate: 55 Kg
604/19/23 Alex Delacroix
2.1) LGS, Lower Fixed Asterism, Design OverviewThe fixed asterisms is adjustable in pitch and yaw about its focus point.The camera assembly is mounted on a gimbal, holding the fold mirror , is bolted on the probe body that also receives the collimator lens
Lateral Fixed Asterism design
Probe (Fold mirror holder)
Focus Lens holderAdjustable 0.25mm per rev.Thorlabs ST1XY-A
Probe Body(Collimator lens holder)Probe Bracket
Tip TiltPI S330-2
Tip Tilt Bracket
Mounting base
Post 1in diaThorlabs RS2 2837-EOW
Field stop(FR-2397)
Collimator Lens holder
Lenslet holder
Relay Lens holder
CCD
Gimbal Assembly
Adjustment KnobNewport AJS100-0.5
Mounting Bolts
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2.2) LGS Fixed Asterism Probe Arm DesignThe Fold mirror is bonded at the extremity of a tubular probe design, bolted to the body, sandwitching the Collimator lens thru a soft o-ring, compressed to hold the lens in place against a machined receptacle.
Probe Arm Assembly (Cross Section)
Probe Mirror(bonded)
Probe Body
Collimator lens
Soft O-ring(Shore A: 50, Buna-N )
Probe Bracket
804/19/23 Alex Delacroix
2.3) LGS Fixed Asterism Gimbal DesignThe Camera assembly is mounted on an aluminium gimbal thru shoulder screws and bronze bushings. The necessary gap and relative position of the gimbal is controlled using shoulder shim stocks.
Gimbal Assembly (Cross Section)
Probe Body
Mounting Base
Shoulder Screw , Stainless SteelØ1/2” x ¾” Lg
Mc Master 94035a503
Gimbal
Sleeve Bearing, flanged, bronzeØ 5/8” OD x Ø 1/2” ID x ½” LgMc Master 7815K29
Shoulder Screw , Stainless SteelØ3/4” x 1-1/4” Lg
Mc Master 90298a837
Sleeve Bearing, flanged, bronzeØ 1” OD x Ø 3/4” ID x 1” LgMc Master 7815K49
Camera Assembly
Shim Stock , Stainless SteelID .501 x .005” +/-.0005” Thk
Mc Master 94773A616
Shim Stock, Stainless SteelID .751” x .020” +/-.0025”
Mc Master 94773A720
904/19/23 Alex Delacroix
2.4) LGS Fixed Asterism Camera Assembly Adjustment DesignThe Camera Assembly pitch and yaw adjustments are located 250mm away from the axis.The 1 inch travel adjustment knobs with a 0.7µm resolution gives the system a 0.57” angular resolution.(tan α = 0.7 E-6 / 250 E-3 = 28 E-7 , α= 160E-6 deg = 0.57 “)
Camera Assembly Adjustment(Cross Section) Mounting Base
Rod, threaded TBD
Camera Assembly
Compression Spring TBD
Adjustment KnobNewport AJS100-0.5
Steel plate
1004/19/23 Alex Delacroix
2.5) LGS, Central Fixed Asterism, Design OverviewThe Central fixed asterism differs in design only by the absence of a probe, rendered unnecessary by it’s central location in the sensor.
Central Fixed AsterismMounting base
Camera Assy
Gimbal Assembly
Fold Mirror
1104/19/23 Alex Delacroix
3) LGS, Patrolling Asterism, Design OverviewPatrolling asterisms are located 120 degrees apart from each other and are pointing the probes toward the 120” FoV
Patrolling Asterism
Patrolling Asterism, upper, left Patrolling Asterism, upper, right
Patrolling Asterism, lower
120” FoV(FR-2362)
Current Mass Estimate: 25 Kg
1204/19/23 Alex Delacroix
3.1) LGS, Patrolling Asterism, Design OverviewThe Patrolling Asterism is composed of two distinct sub assemblies: The Pick off arm Assembly and the Camera Assembly.
Patrolling Asterism
Camera Assembly
Pick off Arm Assembly
Current Mass Estimate: 8 Kg
1304/19/23 Alex Delacroix
3.2) LGS, Patrolling Asterism, Pick Off Arm DesignThe Pick off arm Assembly is composed of three distinct sub assemblies: - The Probe Assembly- The Lever Assembly- The Crank Assembly-The Course limiter pattern is a single part installed at the LGS Assembly level.
Pick off Assembly
Probe Assembly
Lever Assembly
Crank Assembly
Course limiter pattern
3.2.1) LGS, Probe Assembly Optical Design
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a b c d
AO Focus
Collimator Lens (L1)
TT
L2
PO Focus
a1 a2
Probe(FM1)
Lever Arm
OSM# a1 a2= a - a1 a = b = a1 + a2
Arm = b + a2
I 10 110 120 230
II -5 125 120 245
III -20 140 120 260
04/19/23 Alex Delacroix
Table 1
The Pick off arm Assembly is designed to answer the optical equation: a = b & c = d with a + b = x (c + d) and a = a1 + a2
Lever Arm length = b + a2 Solving for a2 2a2 = Lever Arm length - a1 a2 = (Lever Arm length - a1 )/2, so, with a = b = 120
1504/19/23 Alex Delacroix
The Patrolling Asterism is composed of two distinct sub assemblies: The Pick off arm Assembly and the Camera Assembly.
Patrolling Asterism(Cross Section)
Tip Tilt
Collimator Lens
Fold Mirror
Periscope
Focus Lens
3.2.1.1) LGS, Probe Assembly Optical Path
Total Mass: 1,240 grams ( 12.2N )
CG located at the Axis of rotation, 38 mm above the Lever motor Interface.
Torque at the Lever Rotation Stage Interface: 0.038 X 12.2 = 0.46 Nm Well below the manufacturer recommendation of 3 Nm
This gives a Factor of Safety of 3 / 0.46 = 6.5
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½ in dia Collimator Lens1 gram
Tip TiltOIM100
340 grams
Limit Switch Assembly50 grams
CG Location Lever Arm454 grams
04/19/23 Alex Delacroix
Fig. 11
3.2.1.2) Static Load on the Lever Motor
Probe30 gramsCounterweight
300 grams
Total Mass: 3,525 grams (35N)
CG located at the Crank Axis of rotation, 60 mm above the Lever motor Interface.
Torque at the Crank Rotation Stage Interface: 0.060 X 35 = 2.1 Nm Well below the manufacturer recommendation of 6 Nm
This gives a Factor of Safety of 6 / 2.1 = 2.8
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Lever Arm Assembly1,240 grams
Lever Adaptor455 grams
CG Location
Lever MotorPI M-037.DG
650 grams
Crank Adaptor435 grams
Counterweight700 gramsPeriscope Assy
60 grams
04/19/23 Alex Delacroix
3.2.1.3) Static Load on the Crank Motor
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Position Accuracy at the longest probe: OSM #3, a1 = -20
Lever Arm Length: 260mmCrank arm Length: 41.8mm
Lever Stage M-037.DG Design resolution: 0.000034°Crank Stage M-038.DG1 Design resolution : 0.000035°
Lever arm position accuracy: 250mm X tan 0.000034° = 0.00015mm
Crank arm position accuracy: 290mm X tan 0.000035° = 0.00018mm __________
= 0.00033mm = 0.00045”
04/19/23 Alex Delacroix
Fig. 13
Resulting position accuracy at the tip of the probe = 0.00033mm = 0.45 mas
3.2.1.5) Probe Position RepeatabilityPosition Repeatability at the longest probe: OSM #3, a1 = -20
Lever Arm Length: 260mmCrank arm Length: 41.8mm
Lever Stage M-037.DG Design repeatability: 30 μrad = 0.0017°Crank Stage M-038.DG1 Design repeatability : 20 μrad = 0.0011°
Lever arm position repeatability: 250mm X tan 0.0017° = 0.007mmCrank arm position accuracy: 290mm X tan 0.0011° = 0.005mm __________
Resulting Repeatability = 0.012mm = .016” = 16 mas
3.2.1.4) Probe Position Accuracy
FR-2391: Patrolling LGS acquisition accuracy due to absolute positioing accuracy of the OSM shall be better than 100 milliarcseconds
1904/19/23 Alex Delacroix
The Collimator lens, installed inside the Probe body, is held in place by a Soft o-ring installed inside the collimator lens spacer, that is held by the Probe.The Fold mirror is bonded at the tip of the probe.The Probe Assembly needs to be balanced about its axis of rotation to avoit placing uncontrolled loadings on the Lever Rotation Stage.
Probe Arm Assembly(Cross Section)
Limit Switch Assembly
Fold Mirror
Probe
1 inch dia Tip Tilt Optics In Motion 100
3.2.2) LGS, Probe Assembly Mechanical Design
Collimator Lens
Collimator Lens spacer
Probe Body
Soft O-ring(Shore A: 50, Buna-N )
2004/19/23 Alex Delacroix
This device is a wobbler limit switch that gives direction indication.
The wobbler is composed of a Ball Bearing Track Roller (Mc Master 3668K2), a steel shaft mounted on three compression springs, resting on 3 load cells.The load cells give direction and distance measurements.
Operation:Shortly after the arm deviates from its allowed path, the roller will contact the custom track, forcing the spring mounted wobbler base to exercise a pressure on a one or two of the load cells, signaling a trajectory error.Retraction can then be safely done by rotating the crank motor in any direction and rotating the Lever arm in accordance with load cells signals.
WobblerAssembly
3.2.2.1) LGS, Probe Assembly Limit Switch Mechanical Design
Ball Bearing Track RollerMc Master 3668K2
Threaded Steel Shaft
Spring Mounted base
Compression Spring Load cellHoneywell BL912A
Load cellsHoneywell BL912A
2104/19/23 Alex Delacroix
3.2.2.2) LGS, Probe Tip Design
FM1
Probe Tip
Light from Focus
Light to L1
Ellipse Minor Diameter: d = d at Focus Plan + (a1 / f#) = 5 X 0.727 + (20 / 13.66) = 3.635 + 1.464d = 5.10 mm
Ellipse Major Diameter: D = d√2 = 5.1√2 D = 7.21 mm
Ellipse Minor Diameter: d = d at Focus Plan + (a1 / f#) = 5 X 0.727 + (5 / 13.66) = 3.635 + .366d = 4.00 mm
Ellipse Major Diameter: D = d√2 = 4√2 D = 5.66 mm
Ellipse Minor Diameter: d = d at Focus Plan + (a1 / f#) = 5 X 0.727 + (10 / 13.66) = 3.635 + .732d = 4.37 mm
Ellipse Major Diameter: D = d√2 = 4.37√2 D = 6.18 mm
The Field of View at the Focal Plane is Ø 5” (3.635mm)The Field of View at the probe is defined by it’s distance from the Focal Plane / f#The probe Fold Mirror intercept the light beam at a 45 degree angle creating an elliptical projection at a distance a1 from the Focal plane. (See Fig. 4)The minimum diameter of the mirror needs to be larger than the Ellipse Major Diameter.The Larger Fold mirror will be at the furthest distance from the Focal plane OSM #1 (a1 = -20)The Patrolling Asterism LGS WFS channels shall be able to measure wavefronts from two LGS beacons separated by 10 arcseconds. FR-3430
Probe is sized to 8mm Diameter for commonality
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-Mass of the probe w = mg = 0.01 Kg x 9.81 ms-2 = 0.098N
-Moment of Inertia: I = bh3/12 = 4.57 x 7.643/12 = 169.8 mm4
-6061-T6 Module of Elasticity: E = 68,800 N/mm2
-Max Deflection: ν = wL3 / 8EI
ν =0.098 X 1003 / (8 X 68,800 X 169.8)
ν = 98000/ 93457920
ν = 0.001mm
Probe Deflection
Max Probe Deflection, at rest, under it’s own weight: 1µm
• Deflection analyzed on the longest Inclined probe (OSM #2)
Probe Length
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3.2.2.3) LGS, Probe Tip Deflection
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OSM #1
OSM #2
OSM #3
3.2.2.4) LGS, Probe Tip Frequency Analysis
Lowest Frequency
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3.2.3) LGS, Patrolling Asterism, Lever Assembly DesignThe Lever Assembly needs to be balanced about its axis of rotation to avoid uncontrolled loadings on the Crank motor.However, to compensate for undesired backlash of the Lever rotation stage, a slight, almost constant load is applied to the Probe Arm by the Backlash compensating spring system.
Lever Assembly(Cross Section)
Cable WrapEnergy Chain Z045
Backlash compensating spring
Crank Adaptor
Rotation StagePI M-037.DG
Cable Boom
Lever Assembly
Rotation Axis
Lever Adaptor
Periscope
2504/19/23 Alex Delacroix
3.2.4) LGS, Patrolling Asterism, Crank Assembly DesignThe Crank Assembly holds the Crank Rotation Stage, the focus Lens and the Crank Backlash compensating spring system.
Backlash compensating spring
Crank Bracket
Rotation StagePI M-038.DG Folded
Crank Assembly
Focus Lens holder
2604/19/23 Alex Delacroix
3.3) LGS, Patrolling Asterism, Camera Assembly DesignThe Patrolling Asterism Camera Assembly is made of a ¾ in thick Aluminum Honeycomb panel potted with aluminum inserts.It receives the Sensor optical mounts and the Pick off arm assembly.The panel is installed on the LGS Structure through shim stocks for tip tilt adjustment.
Patrolling Asterism, Camera Assembly
Aluminum HoneyComb Panel ¾ in thick
Tip TiltPI S330-2
Collimator Lens holder
Lenslet holder
Relay Lens holder
CCD
Fold Mirror
Three point mount5/16 Bolts and Shim stock
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4) LGS, Structure Design OverviewThe Structure is composed of:- The Plate Structure assembly- The Beam Support Assembly- The Legs Assembly
Pole Assembly
Plate Structure Assembly
Structure Design
Beam Support Assembly
Degree of freedom Criterion Tolerance required
x, y ~ 0.1 arcsec on sky 65 micronsz ~0.1 arcsec spot deflection at
outer subaperture2 mm
qx, qy 15 cm subap / 10 110 micro radiansqz ~0.1 arcsec at 10 arcsec off-
axis radius10 milliradian
X
Y
2804/19/23 Alex Delacroix
4.1) LGS, Plate Structure AssemblyThe Structure, made of 1 inch and ¾ inch Thick bolted Aluminum plates, is rigidly holding each Asterisms. Each channel can be moved individually and locked in place thru a three point mount scheme.Three Hoist Rings are provided for lifting the Assembly with a Crane.
Plate Structure Assembly
Hoist rings
875 mm
616 mm
860 mm
Current Mass Estimate: 90Kg
5/16 Bolts x 1.5in Lg
¼ in Dia Shear pin(Match drilled in place after
assembly and inspection)
2904/19/23 Alex Delacroix
4.2) LGS, Beam Support AssemblyOne side of the Beam Support Assembly carries the LGS Translation mechanism, composed of two Deltron Slide bearings and a motorized stage (FR-2378 ). The other side of the Beam Support Assembly carries the LGS Kinematic Mount Scheme Composed of three receptacles: A Cone, a groove and a Flat. Three Hoist rings are also provided to tie-down the Structure to the telescope Nasmyth.The Beam Support Assembly is made of standard Aluminum IPN and plates Welded.The alignment of the structure relative to the Bench can be done by shimming between this assembly and the Structure assembly.The LGS WFS support structure shall be aligned to the required optical bench interface point to better than 1 mm. FR-2375The LGS WFS support structure shall be aligned to the required optical bench interface optical axis direction to better than 2 arcminutes (physical angle at the interface point) FR-2376
Beam Support Assembly
High Precision Series Crossed Roller Slides10 inches Travel, accuracy .00004 in/in Deltron HPRS 5-10
Current Mass Estimate: 65 Kg
Translation StageNewport MTM250CC
0.1 µm resolution
Tie down Hoist rings
Cone
Groove
Flat
3004/19/23 Alex Delacroix
4.3) LGS, Legs AssemblyThe Legs are the link between the Telescope Nasmyth platform and the LGS structure.They are made of three different materials to compensate for dome temperature variations in conformity with the stability requirement. The LGS WFS support structure shall be stable to a level better than (x,y,z,thetax,thethay,thethaz) = (TBD, TBD, TBD, TBD, TBD, TBD) with respect to the telescope coordinate system. FR-2377
Legs Assembly Current Mass Estimate: 65 Kg
Legs
LGS
Leg Assembly(Cross Section)
Leg Outer shellStainless SteelCTE 14 µm/m/°C
Leg Inner shellAluminiumCTE 25 µm/m/°C
Leg CoreTitaniumCTE 8 µm/m/°C
860 mm
18-8 SS Alu Ti Total Outer Shell Inner Shell Core
Delta T (°C) 40 40 40 Length (m) 0.826 0.775 0.808
CTE (µm/m/°C) 0.000014 0.000025 0.000008 Variation (mm) 0.46256 -0.775 0.25856 -0.05