Agilent 10737L and Agilent 10737R
Compact Three-Axis Interferometers
Chapter 7O Agilent 10737L and Agilent 10737R Compact Three-Axis
Interferometers
Description
Description
NOTEIn this subchapter refers to either or both of the Agilent 10737L and
Agilent 10737R interferometers.
The Agilent 10737L/R Compact Three-Axis interferometers (see
figures 7O-1 through 7O-3) allow up to three measurements
(displacement, pitch, and yaw) to be made on a single axis. The
Agilent 10737L and Agilent 10737R interferometers are identical
except that the “L” bends the measurement beams to the left and the
“R” bends the beams to the right, as viewed from the incoming beam
(see figures 7O-2 and 7O-3).
These interferometers are designed to use a 3 mm diameter laser
beam, available from an Agilent 5517C-003 Laser Head.
The measurement beam parallelism inherent in the design of the
Agilent 10737L/R interferometers ensures that there is essentially no
cosine error between their three measurements and also ensures angle
accuracy for pitch and yaw measurements.
These interferometers are designed for direct attachment of
Agilent 10780F-037 Remote Receiver’s fiber-optic sensor head (one per
axis). The Agilent 10780F-037 receiver is the same as the standard
receiver, except it does not include the lens assembly that attaches to
some Agilent interferometers; in this case, the required lens assembly
is part of the Agilent 10737L/R interferometer. This simplifies user
assembly, since no optical alignment of the recei ve r is required. The
fiber-optic cables from the receivers attach directly to the axis output
apertures on the input face of t he inter feromete r. S ee fi gures 7O-2 and
7O-3.
The Agilent 10737L/R interferometers are based on the
Agilent 10706B High-Stability Plane Mirror Interferometer’s design.
Figure 7O-1 shows two views of an Agilent 10737L interferometer. In
addition to the Agilent 10706B components, the interferometer
includes the following assemblies:
•The receiver assembly. This can be removed during alignment
using the 4-40 socket-head cap screws. The 4-40 button-head
screws hold the 0.100-inch-thick cover plate and the receiver
assembly parts in place; do not try to lo osen these screws or r emove
the plate.
•The shear plate assembly. This assembly is factory-aligned and
must not be loosened or removed.
7O-2User’s Manual
Chapter 7O Agilent 10737L and Agilent 10737R Compact Three-Axis
Interferometers
Description
•The corner cube assembly. This assembly is factory-aligned to
produce the required beam pattern. Do not remove the corner cube
assembly or loosen the screws holding the assembly in place.
Moving this assembly will change the output beam pattern.
Chapter 7O Agilent 10737L and Agilent 10737R Compact Three-Axis
Interferometers
Description
Applications
General
The Agilent 10737L or Agilent 10737R interferometer, by making
three simultaneous distance measurements along or parallel to the
X-axis, can make these measurements:
•displacement along the X-axis
•rotation (pitch) about the Y-axis
•rotation (yaw) about the Z-axis
The angular measurements made by either of these interferometers
can be calculated by taking the arctangent of the difference between
two linear measurements involved, divided by their separation:
–()
YY’
THETAarc
-------------------tan=
D
This method for determining angle is described in more detail in the
“Electronic yaw calculation method” and “Optical yaw calculation
method” subsections under t he “Three-axis system using dis crete plane
mirror interferometers (X, Y, YAW)” section in Chapter 3, “System
Design Considerations,” of this manual.
X-Y Stage
These interferometers are well suited for X-Y stage or multiaxis
applications, such as lithography equipment. Two of these
interferometers, can measure all X, Y, pitch, roll, and yaw motions of a
stage. Since only five axes are required to make all these
measurements, the sixth axis can be used as a redundant yaw
measurement (useful for mirror mapping). In these applications, the
measurement mirrors are attached to the X-Y stage.
7O-6User’s Manual
Chapter 7O Agilent 10737L and Agilent 10737R Compact Three-Axis
ase
ead
g
s
ete
eam
g
s
S
S
s
eter
s
Interferometers
Description
MEASUREMENT USING AGILENT 10737R/L COMPACT
THREE-AXI
Agilent 10737L
Compact Three-axi
Interferom
INTERFEROMETER
To Fiber Optics
Receivers
B
Directin
Optic
L
r H
To Fiber Optics
Receivers
A
ilent 10737R
Compact Three-axi
Interferom
r
Multiaxi
Stage
Figure 7O-4. Measurement using two Agilent 10737R interferometers
Optical Schematics
Optical schematics for these interferometers are given in Figure 7O-5.
Each interferometer functions s i milarly to three parallel
Agilent 10706B High Stability Plane Mirror interferometers with a
three-way beam splitter in front of them.
To reduce thermal drift errors, the measurement and reference beam
paths have the same op t ica l pa th len gt h in gla ss. This mini mi zes
measurement errors due to temper atur e ch anges in t he int erfer ometer .
User’s Manual7O-7
Chapter 7O Agilent 10737L and Agilent 10737R Compact Three-Axis
Interferometers
Description
MEASUREMENT PATH (fB)
Agilent 10737L and Agilent 10737R
Compact Three-Axis Interferometers
f
rom
ase
B
r
Axis #2
Axis #3
F
L
R
eference
M
irro
r
Axis #1 = fB±2 f
Axis #2 = fB±2 f
Axis #3 = fB±2 f
∆
∆
∆
1
2
3
NOTE: Because the Measurement
mirror may have a combination of
displacement, pitch, and yaw motions,
the Measurement Axes may have
different Df values, as shown
Axis #1
M
easuremen
M
irro
r
λ
/4
P
lat
e
t
REFERENCE PATH (fA)
Agilent 10737L and Agilent 10737R
Compact Three-Axis Interferometers
f
rom
ase
r
Axis #1 = f
Axis #2 = f
Axis #3 = f
A
A
A
A
F
L
Axis #2
Axis #3
Axis #1
M
M
R
λ
/4
easuremen
irro
r
eference
M
irro
r
P
lat
e
t
COMPOSITE (fA) and (fB)
Agilent 10737L and Agilent 10737R
Compact Three-Axis Interferometers
f
F
rom
L
ase
B
r
Axis #1 = fB±2 f
Axis #2 = fB±2 f
Axis #3 = fB±2 f