Description

Design Features

AGC motorized mechanical goniometers are used in applications where 90 degrees of angular travel is needed with the payload at the center of rotation, or where two axes of rotation are needed about a common point. AGC goniometers are designed to be mounted to standard optical tables, as well as standard Aerotech rotary stages, to provide roll, pitch, and yaw about a common 3-axis intersection. This flexible stage series is ideal for optical alignment, payload tip/tilt, beam steering, sensor calibration, laser applications, automated manufacturing and/or testing, and multi-axis diffractometer systems.

Construction Features

The sizes within the AGC family are designed to be mounted on one another to form a three-axis rotary system with all three axes of rotation sharing a common intersection point. This allows compact pitch/roll/yaw systems to be created easily from a standard stage platform and without special adapter plates or mating fixtures. The drive mechanism for AGC stages is a precision gear and matched worm that are preloaded to reduce backlash. All AGC stages include optical limit switches and hard stops to define a ±45 degree range of travel.

Innovative feedback technology yields stable performance and negligible performance drift over the life of the stage. This is in stark contrast to inferior designs that must be continually adjusted to compensate for worm wear. All stage tabletops feature hardcoated aluminum, with stainless-steel Heli-Coil® inserts to prevent thread wear.

Flexible Options

Options include flexible motor selections as well as a direct encoder mounted along the stage travel to offer outstanding repeatability and to minimize hysteresis and backlash. Vacuum-compatible versions, for use in pressures as low as 10-6 torr, are also available.

Motor and Drives

Standard AGC stage configurations feature Aerotech’s brushless servomotors. A full range of matching drives and controls are available for a complete single-source solution.

Specifications

Mechanical Specifications

ModelAGC85AGC160AGC245
Travel Range±45°
Accuracy(1)±12 arc sec
Resolution (Minimum Incremental Motion)3 arc sec
Bidirectional Repeatability(1)±10 arc sec
Unidirectional Repeatability(1)±5 arc sec
Tilt Error Motion40 arc sec
Gear Ratio152:1192:1288:1
Maximum Speed30°/s
Nominal Radius of Rotation125 mm200 mm300 mm
Distance from Tabletop to Rotation Point85 mm160 mm245 mm
Maximum Torque (Continuous)18 N-m24 N-m44 N-m
Load Capacity(2)Axial20 kg30 kg50 kg
Moment20 N-m30 N-m50 N-m
Stage Mass5.6 kg12.5 kg24.3 kg
MaterialAluminum Body/Clear Anodize Finish
MTBF (Mean Time Between Failure)5000 Hours
  1. Certified with each stage. Requires direct encoder feedback with calibration option and is tested with Aerotech controller.

  2. On-axis loading is listed.

  3. Specifications are for single-axis systems measured at the center of rotation. Performance of multi-axis systems is payload and workpoint dependent. Consult factory for multi-axis or non-standard applications.

  4. Load Center of Mass not to exceed bounding volume of 160 mm in diameter by 80 mm above pivot point.

Electrical Specifications

ModelAGC85AGC160AGC245
Drive SystemWorm-Gear Assembly
FeedbackRotary Encoder on Drive Motor and Noncontact Direct Encoder
Maximum Bus Voltage320 VDC
Limit Switches5 V, Normally Closed
Home SwitchNear Limit
Motor Line Count (cnts/rev)Analog100010001000
Digital250025005000
Direct Encoder Radius (mm)116.7195.7294.2
Electrical ResolutionMotor EncoderAnalog-Fundamental 
(arc sec)
8.52636.75004.500
Digital 
(arc sec)
0.85260.67500.2250
Direct EncoderAnalog-Fundamental 
(arc sec)
35.349621.079714.0221
Digital x50 
(arc sec)
0.17670.10540.0701

Recommended Controller

ModelAGC85AGC160AGC245
Multi-AxisA3200/NpaqNdrive CP20Ndrive CP20Ndrive CP20
EnsembleEnsemble CP20Ensemble CP20Ensemble CP20
Single AxisSoloistSoloist CP20Soloist CP20Soloist CP20

Dimensions

Ordering Information

AGC Series Gear-Driven Goniometers

OptionDescription
AGC85Gear-driven goniometer, 85 mm radius of curvature
AGC160Gear-driven goniometer, 160 mm radius of curvature
AGC245Gear-driven goniometer, 245 mm radius of curvature

Travel (Required)

OptionDescription
-TR010Limited travel, ±5 degrees
-TR015Limited travel, ±7.5 degrees
-TR020Limited travel, ±10 degrees
-TR025Limited travel, ±12.5 degrees
-TR030Limited travel, ±15 degrees
-TR035Limited travel, ±17.5 degrees
-TR040Limited travel, ±20 degrees
-TR045Limited travel, ±22.5 degrees
-TR050Limited travel, ±25 degrees
-TR060Limited travel, ±30 degrees
-TR070Limited travel, ±35 degrees
-TR080Limited travel, ±40 degrees
-TR090Limited travel, ±45 degrees

Motor (Optional)

OptionDescription
-M1Brushless servomotor with digital encoder; AGC85 (BM75 with 2500-line TTL encoder); AGC160 (BM130 with 2500-line TTL encoder); AGC245 (BM200 with 5000-line TTL encoder)
-M2Brushless servomotor with digital encoder and brake; AGC85 (BM75 with 2500-line TTL encoder); AGC160 (BM130 with 2500-line TTL encoder); AGC245 (BM200 with 5000-line TTL encoder)
-M3Brushless servomotor, 1000-line 1 Vpp encoder; AGC85 (BM75); AGC160 (BM130); AGC245 (BM200)
-M4Brushless servomotor, 1000-line 1 Vpp encoder and brake; AGC85 (BM75); AGC160 (BM130); AGC245 (BM200)

Motor Orientation (Required)

OptionDescription
-2Bottom cable exit, optional orientation
-3Left-side cable exit, standard orientation
-4Top cable exit, optional orientation
-5Right-side cable exit, optional orientation

Direct Rotary Feedback (Optional)

OptionDescription
-E1Incremental encoder, 1 Vpp
-E2Incremental encoder, digital TTL output, x50 multiplication

Note: Using AGC stages with dual feedback loops will necessitate that the drive motor is outfitted with an amplified sine encoder and appropriate encoder interpolation (MXH, MXU or MXR).

Integration (Required)

Aerotech offers both standard and custom integration services to help you get your system fully operational as quickly as possible. The following standard integration options are available for this system. Please consult Aerotech if you are unsure what level of integration is required, or if you desire custom integration support with your system.

OptionDescription
-TASIntegration - Test as system
Testing, integration, and documentation of a group of components as a complete system that will be used together (ex: drive, controller, and stage). This includes parameter file generation, system tuning, and documentation of the system configuration.
-TACIntegration - Test as components
Testing and integration of individual items as discrete components that ship together. This is typically used for spare parts, replacement parts, or items that will not be used together. These components may or may not be part of a larger system.