LCLS Undulator Support/Mover System Testing Status - PowerPoint PPT Presentation

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LCLS Undulator Support/Mover System Testing Status

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Title: LCLS Undulator Support/Mover System Testing Status


1
LCLS Undulator Support/Mover System Testing
Status
  • Jeff T. Collins

2
Support/Mover System Testing
History
  • We Assembled a Breadboard Undulator
    Support/Mover System Using Existing Parts at the
    Early Stages of the Design Process
  • To Get an Early Start on Motion Testing, we
    Specified, Procured and Installed a Very
    Accurate Measurement System for the Breadboard
    Support/Mover System
  • A Labview-Based Data Acquisition and Control
    System was Developed In-House for Command and
    Control of all Motors with Feedback and
    Monitoring from the Measurement System
  • The Breadboard System was Used to Learn How
    to Control and Characterize the Performance of
    the Motion System
  • Results from Numerous Tests were Used as
    Feedback for Refinement of the Design Process.
    Problem Areas have been Identified and Solutions
    have Been Implemented in the Actual
    Support/Mover System Design
  • Measurement Results are Very Encouraging with
    Overall Excellent Repeatability

3
Support/Mover System Testing
4
Support/Mover System Testing
Our Present Breadboard Lacks Many Features
that the Prototype will Include
  • Does not have Expanded Wedge on Upstream
    Double CAM Mover
  • Aluminum Frame instead of Steel Frame
  • Bearing Surfaces are not Hardened or Polished
  • 1001 Gearbox instead of 2501 Gearbox
  • Less Precise Rotary Potentiometers
  • Only Four Linear Potentiometers
  • Lack a Precision Temperature-Controlled
    Environment

5
Support/Mover System Testing
Salient Support/Mover System Physics Requirements
  • Quadrupole Motion Positioning Repeatability 7
    µm
  • Short-Term (1 h) BPM and Quad Stability 2 µm
  • Long-Term (24 h) BPM and Quad Stability 5 µm
  • Horiz. Segment Pos. Repeatability in Roll-Away
    Cycle 10 µm
  • Vert. Segment Pos. Repeatability in Roll-Away
    Cycle 5 µm
  • Quad Transverse Position Change in Roll-Out
    Condition 25 µm
  • Quad Position Reproducibility after Roll-Away
    Cycle 2 µm
  • BPM Transverse Position Change in Roll-Out
    Condition 25 µm
  • BPM Position Reproducibility after Roll-Away
    Cycle 2 µm

6
Support/Mover System Testing
System Measurement Devices
  • Five Keyence Laser Displacement Sensors (0.05
    micron repeatability). Two at each end
    measuring X and Y Displacement at the Quadrupole
    Position, and one located mid-plane of the
    Undulator on one side to measure Roll.
  • Four Linear Potentiometers (1-2 micron
    repeatability) measuring X and Y Displacements
    on one side of the Girder located near the CAM
    Movers.

7
Support/Mover System Testing
8
Support/Mover System Testing
CAM Mover System Degrees of Freedom
  • X-Translation (Inboard or Outboard Translation)
  • Y- Translation (Up or Down Translation)
  • Pitch Motion (Upstream or Downstream Pitch)
  • Roll Motion (Inboard or Outboard Roll)
  • Yaw Motion (From Either End or Both Ends)
  • Notes
  • The System can Move with Five Degrees of Freedom
    using any Combination of these Motions.
  • The Z-Dimension is Restricted but not
    Constrained via the Recessed Flat on the Single
    CAM Mover.

9
Support/Mover System Testing
CAM Mover Calibration Procedure
  1. Rotate one CAM through a Full Revolution
  2. Measure Displacement as a function of Angular
    Position using either the Keyence Sensors or the
    Linear Potentiometers
  3. Plot the Displacement as a function of Angular
    Position
  4. Curve Fit the Data to Locate the Zero Position
  5. Repeat this Process for each of the Five CAM
    Movers

Problems with this Approach
  • Rotating one CAM introduces Pitch, Roll, and Yaw
    into the System
  • These Motions add Stress into the Girder causing
    Distortion
  • These Distortions become part of the Calibration
  • The Calibration is not Decoupled from the Girder
  • The existing Rotary Potentiometers have 1 of
    Backlash adding to
  • Calibration Uncertainty

10
Support/Mover System Testing
11
Case 1 X-Translation /- 1.5 mm Cyclic Motion
Repeatability
Location Laser Displacement Sensors Linear Potentiometers
Upstream X 2.5 µm 1.5 µm
Upstream Y 1.0 µm 4.0 µm
Downstream X 2.0 µm 2.5 µm
Downstream Y 0.5 µm 4.0 µm
Target Repeatability lt /- 7.0 µm
12
Support/Mover System Testing
Infrared Image Prior to Motor Operation,
Downstream End Double CAM Mover with Pedestal
Base
13
Support/Mover System Testing
Infrared Image Prior to Motor Operation,
Downstream End Double CAM Mover with Pedestal
Base
14
Support/Mover System Testing
Infrared Image After Motor Operation, Downstream
End Double CAM Mover with Pedestal Base, Motor on
for Approximately 2 Hours
15
Case 2 Y-Translation /- 1.5 mm Cyclic Motion
Repeatability
Location Laser Displacement Sensors Linear Potentiometers
Upstream X 1.0 µm 2.5 µm
Upstream Y 2.5 µm 1.0 µm
Downstream X 0.5 µm 4.0 µm
Downstream Y 1.5 µm 1.0 µm
Target Repeatability lt /- 7.0 µm
16
Case 3 Roll /- 1.5 mm Cyclic Motion
Repeatability
Location Laser Displacement Sensors Linear Potentiometers
Upstream X 1.0 µm 2.0 µm
Upstream Y 0.5 µm 0.5 µm
Downstream X 0.5 µm 4.0 µm
Downstream Y 0.5 µm 1.5 µm
Target Repeatability lt /- 7.0 µm
17
Case 4 Upstream Pitch /- 1.5 mm Cyclic Motion
Repeatability
Location Laser Displacement Sensors Linear Potentiometers
Upstream X 1.0 µm 2.0 µm
Upstream Y 1.5 µm 1.0 µm
Downstream X 0.5 µm 2.0 µm
Downstream Y 0.5 µm 0.5 µm
Target Repeatability lt /- 7.0 µm
18
Case 5 Both Ends Yaw 1.5 mm in Opposite
Directions
Location Laser Displacement Sensors Linear Potentiometers
Upstream X 15.0 µm 2.5 µm
Upstream Y 5.0 µm 2.5 µm
Downstream X 25.0 µm 2.5 µm
Downstream Y 2.5 µm 5.0 µm
Target Repeatability lt /- 7.0 µm
Note
Yaw Motion is Incidental and is Not Required for
Actual Operation.
19
Support/Mover System Testing
CAM Mover System Observations
  • All Motions that allow the CAM Bearings to Freely
    Rotate (X-Translation, Y-Translation, and Roll)
    are Repeatable to better than /- 2.5 microns at
    the Quadrupole Position (Target Repeatability lt
    /- 7.0 microns).
  • Though Pitch Motion is Overconstrained the
    Bearing on the Single CAM Mover only needs to
    Slip a few microns Across the Recessed Flat and
    therefore the Motion still Shows Excellent
    Repeatability.
  • Yaw Motion is very Overconstrained and therefore
    the Bearing on the Single CAM Mover Must Slip
    Hundreds of microns Across the Recessed Flat.
    This Slippage, the Process of Overcoming Static
    Friction, Distorts the Girder Causing Large
    Repeatability Errors.

20
Support/Mover System Testing
CAM Mover System Observations
  • Some Repeatability Error is Added to the Linear
    Potentiometers
  • from Sliding Across the Contact Surfaces causing
    Bending of the
  • Sensor Arms.
  • The Ball Bearing Tips of the Linear
  • Potentiometers Wore Flat after Many
  • Cycles from Sliding Across the Contact
  • Surfaces.
  1. From a Cold Start, Heat from the Motors can Cause
    Tens of Microns of Change from the Original Start
    Position.

21
Undulator Roll-Away Cycle Testing
Undulator Segment Roll-Away Cycle /- 10 mm
Cyclic Translation
Note Translation Stage Motions were Driven
Purely by Motor Steps with no Feedback from the
Linear Encoders. Many Changes will be Made to
these Stages for the Actual Prototype.
22
Implemented Changes for the Actual Prototype
  1. Improved Translation Stage Design for Roll-Away
    Cycle
  • Stages will be Preloaded to Decrease Play in the
    Slides
  • Gearboxes Replaced with GAM Angular Gearboxes
    with Backlash Less than 15 arcsec. (Compared to
    40 arcsec. on Existing Stages)
  • Table Length Increased from 6 to 8 and Ball
    Bearing Separation is Increased Accordingly
  • Size of all Mounting Holes have been Increased
    for Added Stiffness

23
Implemented Changes for the Actual Prototype
  1. Steel Girder Replaces the Aluminum Girder.

24
Implemented Changes for the Actual Prototype
  • Expanded Wedge on the Upstream Double CAM Mover
    for
  • Increased Stability.

25
Implemented Changes for the Actual Prototype
  • Inverted Wedge for the Single CAM Mover to
    Constrain Z-Dimension
  • Movement.

26
Implemented Changes for the Actual Prototype
  1. Two Side-by-Side Bearings for the Single CAM
    Mover to Eliminate Slip across the Bearing
    Surface.

27
Implemented Changes for the Actual Prototype
  • Spherical Bearings for Both of the Double CAM
    Movers to allow
  • Rotational Play on these Bearings. The Single
    CAM Mover will
  • still use a Roller Bearing. High Precision
    Bearings will Replace the
  • Existing Standard Bearings.

Note Changes to the Bearings on the Double CAM
Movers, the Inverted Wedge Bearing Surface,
and the Side-by-Side Bearings on the Single CAM
Mover will Eliminate Bearing Slip and will
Allow the Girder to Pivot about the Single CAM
Mover Contact Surface.
28
Implemented Changes for the Actual Prototype
  1. The Addition of Four more Linear Potentiometers
    to Provide X and Y Displacement Information at
    the Four Corners of the Girder near the CAM
    Movers.

Note With Eight Linear Potentiometers Defining
the Girder Position, the Effects of Girder
Distortion can be Decoupled from the CAM Mover
Calibrations allowing Precise CAM Mover
Calibration.
29
Implemented Changes for the Actual Prototype
  1. Replace the 1001 Gearboxes with 2501 Gearboxes.
    This will Eliminate the need for Brakes on the
    Motors, add Better Resolution to the System, and
    Simplify Control System.
  2. Replace existing Rotary Potentiometers (1
    Backlash) with more Precise Rotary Potentiometers
    with better than 0.1 Backlash. This will
    Improve CAM Mover Calibration.
  3. All Bearing Surfaces shall be Hardened and Highly
    Polished. This should add to Long-Term System
    Stability and Repeatability.

30
Support/Mover System Testing
Conclusions
  • The LCLS Undulator Support/Mover Tests on our
    Breadboard are Very Encouraging with Overall
    Excellent Repeatability.
  • We have Identified Problem Areas and have
    Implemented Solutions that will Improve
    Performance.
  • Testing To-Date has Provided Valuable Information
    on System Dynamics, Environmental Influences,
    Calibration Procedures, and Feedback and Control
    Algorithms.
  • Similar, but more in-depth, Tests shall be
    Performed on the Actual Prototype once the System
    has been Assembled.
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