Aerotech Soloist CP Series Hardware Manual
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Aerotech Soloist CP Series Hardware Manual

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Soloist CP Hardware Manual
Revision: 4.09.00

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Summary of Contents for Aerotech Soloist CP Series

  • Page 1: Soloist Cp Hardware Manual

    Soloist CP Hardware Manual Revision: 4.09.00...
  • Page 2 This manual contains proprietary information and may not be reproduced, disclosed, or used in whole or in part without the express written permission of Aerotech, Inc. Product names mentioned herein are used for identification purposes only and may be trademarks of their respective companies.

  • Page 3: Table Of Contents

    2.5. Auxiliary I/O Connector (J104) 2.5.1. Auxiliary Encoder Channel (J104) 2.5.2. Position Synchronized Output (PSO)/Laser Firing (J104) 2.5.3. Digital Outputs (J104) 2.5.4. Digital Inputs (J104) 2.5.5. High-Speed User Inputs 4-5 (J104) 2.5.6. Analog Output 0 (J104) 2.5.7. Differential Analog Input 0 (J104) www.aerotech.com...
  • Page 4 3.4. User Power (TB204, TB205) 3.5. Relay Connector (TB206) Chapter 4: Standard Interconnection Cables 4.1. Joystick Interface 4.2. Handwheel Interface Chapter 5: Maintenance 5.1. Control Board 5.2. Preventative Maintenance Appendix A: Warranty and Field Service Appendix B: Revision History Index www.aerotech.com...

  • Page 5: List Of Figures

    Analog Output 0 (J104) Figure 2-41: Analog Input 0 (J104) Figure 2-42: Brake Connected to J103 Figure 2-43: Brake Connected to TB103 Figure 2-44: RS-232 Interface (TB103) Figure 3-1: Soloist CP with -IO Option Board Figure 3-2: Analog Output Connector (TB201) www.aerotech.com...
  • Page 6 Two Axis Joystick Interface (to the Aux I/O and I/O Board) Figure 4-4: Two Axis Joystick Interface (to the I/O board of two drives) Figure 4-5: Handwheel Interconnection (to Aux I/O) Figure 4-6: Handwheel Interconnection (to Aux I/O via a BBA32 Module) Figure 5-1: Control Board Assembly www.aerotech.com...

  • Page 7: List Of Tables

    Motor Power Output Connections (TB102) Table 2-10: Mating Connector Part Numbers for the Motor Power Output Connector Table 2-11: Wire Colors for Aerotech Supplied Cables (Brushless)  Table 2-12: Wire Colors for Aerotech Supplied Cables (DC Brush)   Table 2-13: Wire Colors for Aerotech Supplied Cables (Stepper)   ...
  • Page 8 Table 3-22: -IO Expansion Board Brake Jumper Configuration  Table 4-1: Standard Interconnection Cables Table 4-2: Cable Part Numbers Table 5-1: LED Description Table 5-2: Control Board Jumper Configuration  Table 5-3: Control Board Fuse Information  Table 5-4: LED Description Table 5-5: Preventative Maintenance www.aerotech.com...

  • Page 9: Eu Declaration Of Conformity

    Declaration of Conformity Soloist CP EU Declaration of Conformity Manufacturer Aerotech, Inc. Address 101 Zeta Drive Pittsburgh, PA 15238-2811 Product Soloist CP Model/Types This is to certify that the aforementioned product is in accordance with the applicable requirements of the...

  • Page 10: Agency Approvals

    Soloist CP Declaration of Conformity Agency Approvals Aerotech, Inc. Model Soloist CP Series Digital Drives have been tested and found to be in accordance to the following listed Agency Approvals: Approval / Certification: CUS NRTL Approving Agency: TUV SUD America Inc.

  • Page 11: Safety Procedures And Warnings

    N O T E : Aerotech continually improves its product offerings; listed options may be superseded at any time. All drawings and illustrations are for reference only and were complete and accurate as of this manual’s release.
  • Page 12 4. Do not expose this product to environments or conditions outside of the listed specifications. Exceeding environmental or operating specifications can cause damage to the equipment. 5. Operators must be trained before operating this equipment. 6. All service and maintenance must be performed by qualified personnel. www.aerotech.com...

  • Page 13: Quick Installation Guide

    Section 2.2. Motor Output Connections Motor Feedback Section 2.3. Motor Feedback Connections (J103) Ethernet / USB No Section / Standard Connection Control Supply Section 2.1.1. Control Supply Connections (TB106) Motor Supply Section 2.1.2. Motor Supply Connections (TB102) Additional I/O User / Application dependent www.aerotech.com...
  • Page 14 Soloist CP Quick Installation Guide This page intentionally left blank. www.aerotech.com...

  • Page 15: Chapter 1: Introduction

    Soloist CP Chapter 1: Introduction Aerotech’s Soloist CP (Compact PWM) network digital drive is a high performance amplifier. The drive provides deterministic behavior, auto-identification, and easy software setup. The Soloist CP’s high performance double precision floating point DSP controls the digital PID and current loops. All system configuration is done using software-settable parameters, including control loop gains and system safety functions.

  • Page 16: Table 1-1: Feature Summary

    Refer to the Help file. Locked drive; firmware and calibration data on the drive cannot be modified by the -LCK user; the drive must be returned if updates are required; read/write access to parameters and programs is supported Chapter 1 www.aerotech.com...

  • Page 17: Figure 1-2: Functional Diagram

    Introduction Soloist CP The following block diagram shows a connection summary. For detailed connection information, refer to Chapter 2 and Chapter 3. Figure 1-2: Functional Diagram www.aerotech.com Chapter 1...

  • Page 18: Drive And Software Compatibility

    Drives that list a specific version number in the Last Software Version column will not be supported after the listed version. Table 1-3: Drive and Software Compatibility Drive Type Firmware Revision First Software Version Last Software Version 1.00 Current 2.01 Current 2.54 Current Chapter 1 www.aerotech.com...

  • Page 19: Electrical Specifications

    Over temperature; Control power supply under voltage; Power stage bias supply under voltage Isolation Optical and transformer isolation between control and power stages. (1) AC input voltage and load dependent.  (2) Dependent on total output power: efficiency increases with increasing output power. www.aerotech.com Chapter 1...

  • Page 20: System Power Requirements

    Ploss = 3 * I(rms)^2 * R(line-line)/2 Pin = SUM ( Pout + Ploss ) / EfficiencyFactor DC Brush Motor Pout [W] = Torque [N·m] * Angular velocity[rad/sec] Ploss = I(rms)^2 * R Pin = SUM ( Pout + Ploss ) / EfficiencyFactor Chapter 1 www.aerotech.com...

  • Page 21: Power Dissipation

    Figure 1-3: Power Dissipation vs. Output Current  Figure 1-4: Ambient Temperature vs. Power Dissipation EXAMPLE:  320 VDC Bus operation at 5 A Power Dissipation = 47 Watts Maximum Ambient Temperature = 54°C www.aerotech.com Chapter 1...

  • Page 22: Mechanical Design

    25 mm (1") of free air space. A space of 100 mm (4") should be allowed along the front of the unit for cable connections. Figure 1-5: Dimensions Table 1-5: Physical Specifications Weight Standard 1.63 kg (3.6 lb) Chapter 1 www.aerotech.com...

  • Page 23: Environmental Specifications

    Maximum relative humidity is 80% for temperatures up to 31°C. Decreasing Humidity linearly to 50% relative humidity at 40°C. Non condensing. Altitude Up to 2000 meters. Pollution Pollution degree 2 (normally only non-conductive pollution). Indoor use only. www.aerotech.com Chapter 1...
  • Page 24 Soloist CP Introduction This page intentionally left blank. Chapter 1 www.aerotech.com...

  • Page 25: Chapter 2: Installation And Configuration

    The Soloist CP has two AC input connectors; one for control power and a second for motor power. For a complete list of electrical specifications, refer to Section 1.2. N O T E : The machine integrator, OEM or end user is responsible for meeting the final protective ground- ing requirements of the system. www.aerotech.com Chapter 2...

  • Page 26: Control Supply Connections (Tb106)

    Neutral if an external 2 A time-delay fuse is used. Although the control power supply contains an internal filter, an additional external filter located as close as possible to the Soloist CP may be required for CE compliance (Aerotech recommends Schaffner FN2080 or Aerotech UFM-ST).

  • Page 27: Motor Supply Connections (Tb102)

    (1) Refer to local electrical safety requirements to correctly size external system wires. Table 2-4: Mating Connector Part Numbers for the Motor Supply Connector Tightening Wire Size: Torque (Nm) Description Aerotech P/N Phoenix P/N [AWG] 7-Pin Terminal Block ECK01114 1754546 0.5 - 0.6 3.3 - 0.516 [12-30]...

  • Page 28: Transformer Options

    80 VDC power bus. 1.5 kVA, 2.5 kVA, or 5 kVA isolation transformer; 115/230 VAC input; 28, 43, 56, TV1.5, TV2.5, or TV5 70, 115 VAC output Figure 2-3: Transformer Examples Chapter 2 www.aerotech.com...

  • Page 29: Vdc Motor Power With A Tv0.3-28-56-St Transformer

    Installation and Configuration Soloist CP Figure 2-4: 40 VDC Motor Power with a TV0.3-28-56-ST Transformer www.aerotech.com Chapter 2...

  • Page 30: Vdc Motor Power With A Tv0.3-28-56-St Transformer

    Soloist CP Installation and Configuration Figure 2-5: 80 VDC Motor Power with a TV0.3-28-56-ST Transformer Chapter 2 www.aerotech.com...

  • Page 31: Volt Dc Bus From 115 And 230 Vac Source

    Installation and Configuration Soloist CP Figure 2-6: 40 Volt DC Bus from 115 and 230 VAC Source www.aerotech.com Chapter 2...
  • Page 32 Soloist CP Installation and Configuration Figure 2-7: 80 Volt DC Bus from 115 and 230 VAC Source (TV0.3-56) Chapter 2 www.aerotech.com...
  • Page 33 Installation and Configuration Soloist CP Figure 2-8: 160 Volt DC Bus from 115 and 230 VAC Source (TV0.3-56) www.aerotech.com Chapter 2...

  • Page 34: Figure 2-9: Control And Motor Power Wiring Using A Tm3 Or Tm5 Transformer

    Soloist CP Installation and Configuration Figure 2-9: Control and Motor Power Wiring using a TM3 or TM5 Transformer Chapter 2 www.aerotech.com...

  • Page 35: Minimizing Conducted, Radiated, And System Noise

    0.5 mm (#20 AWG) EIZ01001 #2673000801 Elna Fair-Rite Products Aerotech's UFM-ST AC line filter and isolation transformers connected to the motor supply AC input are also effective in reducing PWM generated noise and improving performance (refer to Section 2.1.3.). Table 2-8: UFM-ST Electrical Specifications ...

  • Page 36: Motor Output Connections

    Earth Ground to Motor (required for safety) Table 2-10:  Mating Connector Part Numbers for the Motor Power Output Connector Tightening Wire Size: Torque (Nm) Description Aerotech P/N Phoenix P/N [AWG] 7-Pin Terminal Block ECK01114 1754546 0.5 - 0.6 3.3 - 0.516 [12-30] Chapter 2 www.aerotech.com...

  • Page 37: Brushless Motor Connections

    Refer to Section 2.2.1.1. for powered motor phasing or Section 2.2.1.2. for unpowered motor and feedback phasing. N O T E :  If using standard Aerotech motors and cables, motor and encoder connection adjustments are not required. www.aerotech.com Chapter 2...

  • Page 38: Powered Motor Phasing

    Soloist CP Installation and Configuration 2.2.1.1. Powered Motor Phasing Refer to the Motor Phasing Calculator in the Configuration Manager for motor, Hall, and encoder phasing. Figure 2-12: Encoder and Hall Signal Diagnostics Chapter 2 www.aerotech.com...

  • Page 39: Unpowered Motor And Feedback Phasing

    With the designations of the motor and Hall leads of a third party motor determined, the motor can now be connected to an Aerotech system. Connect motor lead A to motor connector A, motor lead B to motor connector B, and motor lead C to motor connector C. Hall leads should also be connected to their respective feedback connector pins (Hall A lead to the Hall A feedback pin, Hall B to Hall B, and Hall C to Hall C).

  • Page 40: Dc Brush Motor Connections

    Red & Orange Yellow & Blue Black Yellow & Blue (1) Wire Color Set #1 is the typical Aerotech wire set used by Aerotech. (2) “&” (Red & Orange) indicates two wires; “ / ” (Green/White) indicates a single wire Chapter 2 www.aerotech.com...

  • Page 41: Dc Brush Motor Phasing

    5. Connect the motor lead from the voltmeter to the ØA motor terminal on the Soloist CP. Connect the motor lead from the negative lead of the voltmeter to the ØC motor terminal on the Soloist CP. N O T E : If using standard Aerotech motors and cables, motor and encoder connection adjustments are not required.

  • Page 42: Stepper Motor Connections

    Green/Yellow & Shield Black Brown Yellow White White & Red (1) Wire Color Set #1 is the typical Aerotech wire set used by Aerotech. (2) “&” (Red & Orange) indicates two wires; “ / ” (Green/White) indicates a single wire Chapter 2 www.aerotech.com...

  • Page 43: Stepper Motor Phasing

    Figure 2-18: Clockwise Motor Rotation N O T E : If using standard Aerotech motors and cables, motor and encoder connection adjustments are not required. N O T E :  After the motor has been phased, use the ReverseMotionDirection parameter to change the dir- ection of “positive”...

  • Page 44: Motor Feedback Connections (J103)

    Input Counterclockwise End of Travel Limit Input Brake Output + Output Table 2-15: Mating Connector Part Numbers for the Motor Feedback Connector (J103) Mating Connector Aerotech P/N Third Party P/N 25-Pin D-Connector ECK00101 FCI DB25P064TXLF Backshell ECK00656 Amphenol 17E-1726-2 Chapter 2...

  • Page 45: Encoder Interface (J103)

    Absolute Encoder Interface Clock - Output Encoder Marker Reference Pulse + Input Absolute Encoder Interface Clock + Output Encoder Cosine + Input Encoder Cosine - Input Encoder Sine + Input Encoder Sine - Input Signal Common for Encoder www.aerotech.com Chapter 2...

  • Page 46: Line Driver Encoder (Standard)

    An analog encoder is used with the -MXU option (refer to Section 2.3.1.3. for more information). Table 2-17: Encoder Specifications Specification Value Encoder Frequency 10 MHz maximum (25 nsec minimum edge separation) x4 Quadrature Decoding 40 million counts/sec Figure 2-19: Line Driver Encoder Interface (J103) Chapter 2 www.aerotech.com...

  • Page 47: Absolute Encoder Interface (J103)

    Section 2.3.1. N O T E :  The PSO feature is not compatible with the -MXU option. The PSO feature operates with the - MXH option and with square wave encoders. Figure 2-20: Serial Data Stream Interface www.aerotech.com Chapter 2...

  • Page 48: Analog Encoder Interface

    Analog Encoder Phasing Reference Diagram N O T E : The input amplitude is measured peak to peak for any encoder signal (sin, sin-n, cos, cos-n) relative to signal common. These signals have a typical offset voltage of 2V to 2.5V. Chapter 2 www.aerotech.com...

  • Page 49: Figure 2-22: Analog Encoder Interface (J103)

    Installation and Configuration Soloist CP Figure 2-22: Analog Encoder Interface (J103) www.aerotech.com Chapter 2...

  • Page 50: Encoder Phasing

    Figure 2-23: Encoder Phasing Reference Diagram (Standard) N O T E :  Encoder manufacturers may refer to the encoder signals as A, B, and Z. The proper phase rela- tionship between signals is shown in Figure 2-23. Chapter 2 www.aerotech.com...

  • Page 51: Figure 2-24: Position Feedback In The Diagnostic Display

    Installation and Configuration Soloist CP Figure 2-24: Position Feedback in the Diagnostic Display www.aerotech.com Chapter 2...

  • Page 52: Hall-Effect Interface (J103)

    +5V Power for Encoder (500 mA max) Output Hall-Effect Sensor B (brushless motors only) Input Hall-Effect Sensor A (brushless motors only) Input Hall-Effect Sensor C (brushless motors only) Input Signal Common for Encoder Figure 2-25: Hall-Effect Inputs (J103) Chapter 2 www.aerotech.com...

  • Page 53: Thermistor Interface (J103)

    The nominal trip value of the sensor is 1k Ohm. Table 2-20: Thermistor Interface Pin on the Motor Feedback Connector (J103) Pin# Description In/Out/Bi Motor Over Temperature Thermistor Input Figure 2-26: Thermistor Interface Input (J103) www.aerotech.com Chapter 2...

  • Page 54: Encoder Fault Interface (J103)

    Table 2-21: Encoder Fault Interface Pin on the Motor Feedback Connector (J103) Pin# Description In/Out/Bi Encoder Fault Input Input Figure 2-27: Encoder Fault Interface Input (J103) Chapter 2 www.aerotech.com...

  • Page 55: End Of Travel Limit Input Interface (J103)

    End of Travel Limit Input Interface Pins on the Motor Feedback Connector (J103) Pin# Description In/Out/Bi Clockwise End of Travel Limit Input +5V Power for Limit Switches (500 mA max) Output Signal Common for Limit Switches Home Switch Input Input Counterclockwise End of Travel Limit Input www.aerotech.com Chapter 2...

  • Page 56: Figure 2-29: End Of Travel Limit Interface Input (J103)

    Soloist CP Installation and Configuration Figure 2-29: End of Travel Limit Interface Input (J103) Chapter 2 www.aerotech.com...

  • Page 57: End Of Travel Limit Phasing

    CW and CCW inputs at the motor feedback connector. The logic level of the EOT limit inputs may be viewed in the Diagnostic Display (shown in Figure 2-30). Figure 2-30: Limit Input Diagnostic Display www.aerotech.com Chapter 2...

  • Page 58: Brake Output (J103)

    Refer to Section 3.5. for more information on using the brake output with the mechanical relay. Table 2-23: Brake Output Pins on the Motor Feedback Connector (J103) Pin# Description In/Out/Bi Brake Output - Output Brake Output + Output Chapter 2 www.aerotech.com...

  • Page 59: Emergency Stop Sense Input Connector (Tb101)

    Table 2-24. These devices are applied across the switched coil to suppress transient voltages. Table 2-24: Electrical Noise Suppression Devices Device Aerotech P/N Third Party P/N RC (.1uf / 200 ohm) Network EIC00240 Electrocube RG1782-8 Varistor EID00160...

  • Page 60: Typical Estop Interface

    The external relay must be sized based on the number of the Soloist CPs connected and the peak current rating of each drive. Figure 2-32: Typical Emergency Stop Circuit Table 2-26: Typical ESTOP Relay Ratings Axes Aerotech P/N Third Party P/N ECW1018 Sprecher & Schuh CA7-16C-xx-xxx 2 to 5 ECW1019 Sprecher & Schuh CA7-43C-xx-xxx Chapter 2 www.aerotech.com...

  • Page 61: Auxiliary I/O Connector (J104)

    Table 2-28: Mating Connector Part Numbers for the Auxiliary I/O Connector (J104) Mating Connector Aerotech P/N Third Party P/N Connector ECK01259 Kycon K86-AA-26P Backshell ECK01022 Amphenol 17E-1725-2 NOTE: These items are provided as a set under the Aerotech P/N: MCK-26HDD. www.aerotech.com Chapter 2...

  • Page 62: Auxiliary Encoder Channel (J104)

    Auxiliary Cosine+ Bidirectional Auxiliary Cosine- Bidirectional +5 Volt (500 mA max) Output Auxiliary Marker- / PSO output Bidirectional Auxiliary Marker+ / PSO output Bidirectional Common (+5 Volt User Supply, 500 mA max) (2) For PSO, see Section 2.5.2. Chapter 2 www.aerotech.com...

  • Page 63: Figure 2-33: Auxiliary Encoder Channel (J104)

    Installation and Configuration Soloist CP Figure 2-33: Auxiliary Encoder Channel (J104) www.aerotech.com Chapter 2...

  • Page 64: Position Synchronized Output (Pso)/Laser Firing (J104)

    N O T E :  The PSO feature is not compatible with the -MXU option. The PSO feature operates with the - MXH option and with square wave encoders. Table 2-32: PSO Output Pins on the Auxiliary I/O Connector (J104) Pin# Description In/Out/Bi Auxiliary Marker- / PSO output Bidirectional Auxiliary Marker+ / PSO output Bidirectional Analog Common Chapter 2 www.aerotech.com...

  • Page 65: Figure 2-34: Pso Interface

    Installation and Configuration Soloist CP Figure 2-34: PSO Interface www.aerotech.com Chapter 2...

  • Page 66: Digital Outputs (J104)

    Output Off (High Impedance State) Table 2-34: Port 0 Digital Output Connector Pins on the Auxiliary I/O Connector (J104) Pin# Description In/Out/Bi Digital Output 0 Output Digital Output 1 Output Digital Output 2 Output Output Common Digital Output 3 Output Chapter 2 www.aerotech.com...

  • Page 67: Figure 2-35: Outputs Connected In Current Sourcing Mode (J104)

    Installation and Configuration Soloist CP N O T E : Outputs must be connected as all sourcing or all sinking. Figure 2-35: Outputs Connected in Current Sourcing Mode (J104) Figure 2-36: Outputs Connected in Current Sinking Mode (J104) www.aerotech.com Chapter 2...

  • Page 68: Digital Inputs (J104)

    Port 0 Digital Input Connector Pins on the Auxiliary I/O Connector (J104) Pin# Description In/Out/Bi Digital Input 0 / CCW EOT Input Input Digital Input 1 / CW EOT Input Input Input Common Digital Input 2 / Home Input Input Digital Input 3 Input (1) Software configured option Chapter 2 www.aerotech.com...

  • Page 69: Figure 2-37: Inputs Connected In Current Sourcing Mode (J104)

    N O T E : Each bank of 8 Inputs must be connected in the all sourcing or all sinking configuration. Figure 2-37: Inputs Connected in Current Sourcing Mode (J104) Figure 2-38: Inputs Connected in Current Sinking Mode (J104) www.aerotech.com Chapter 2...

  • Page 70: High-Speed User Inputs 4-5 (J104)

    No shunt option present Shunt option present 24 V operation (High Speed Input 4) 5 V operation (High Speed Input 4) 24 V operation (High Speed Input 5) 5 V operation (High Speed Input 5) 1. Default Figure 2-39: High-Speed User Inputs (J104) Chapter 2 www.aerotech.com...

  • Page 71: Analog Output 0 (J104)

    Output Current 5 mA Resolution (bits) 16 bits Resolution (volts) 305 µV Table 2-41: Analog Output Connector Pins on the Auxiliary I/O Connector (J104) Pin# Description In/Out/Bi Analog Output 0 Output Analog Common Figure 2-40: Analog Output 0 (J104) www.aerotech.com Chapter 2...

  • Page 72: Differential Analog Input 0 (J104)

    1. Signals outside of this range may damage the input Table 2-43: Analog Input Connector Pins on the Auxiliary I/O Connector (J104) Pin# Description In/Out/Bi Analog Input 0 + (Differential) Input Analog Input 0- (Differential) Input Analog Common Figure 2-41: Analog Input 0 (J104) Chapter 2 www.aerotech.com...

  • Page 73: Brake Power Supply Connector (Tb103)

    Brake Power Supply (-) Input Brake Power Supply (+) Input Table 2-46: Mating Connector Part Numbers for the Brake Power Supply Connector (TB103) Wire Size: Description Aerotech P/N Phoenix P/N AWG [mm 6-Pin Terminal Block ECK01364 1881367 0.5 - 0.080 [20-28] www.aerotech.com...

  • Page 74: Figure 2-42: Brake Connected To J103

    +24 VDC brake connected to the Motor Feedback connector. In this example the external +24 VDC power source is connected to TB103. Figure 2-42: Brake Connected to J103 N O T E :   The user is responsible for providing fuse protection for the brake circuit. Chapter 2 www.aerotech.com...

  • Page 75: Figure 2-43: Brake Connected To Tb103

    24 VDC brake connected to TB103. The user must connect J103 pin 13 to J103 pin 25. In this case, J103 would function as an interlock to prevent the brake from releasing if the Motor Feedback connector is not connected. Figure 2-43: Brake Connected to TB103 www.aerotech.com Chapter 2...

  • Page 76: Interface (Tb103)

    Brake Power Supply + Output (1) Total user +5 V power is limited to 500 mA. Table 2-48: RS-232 Port Connector Mating Connector (TB103) Tightening Type Aerotech P/N Phoenix P/N Torque (Nm) Wire Size: mm [AWG] 6-Pin Terminal Block ECK01364 1881367 0.5 - 0.080 [20-28]...

  • Page 77: Extshunt Option (Tb104)

    It must be properly enclosed and shielded to avoid risk of fire and operator shock. Table 2-49: -EXTSHUNT Component Information Component Description Aerotech P/N 50 Ω (min), 300 W Recommended Shunt Resistor ECR01039 Vishay/Dale: RBEF030050R00KFBVT Screw Torque Value: 0.5 - 0.6 N·m Wire Size: 12-30 AWG [3.3 - 0.0516 mm...
  • Page 78 (W) time between deceleration events (s) CYCLE Equation 5:    hysteresis voltage of regeneration circuit (V) [10 V, Typical] Additional useful equations: 1 lb·ft = 1.356 N·m 1 rad/s = 9.55 rpm Chapter 2 www.aerotech.com...

  • Page 79: Pc Configuration And Operation Information

    Installation and Configuration Soloist CP 2.9. PC Configuration and Operation Information For additional information about PC configuration, hardware requirements, programming, utilities, and system operation refer to the Soloist Help file. www.aerotech.com Chapter 2...
  • Page 80 Soloist CP Installation and Configuration This page intentionally left blank. Chapter 2 www.aerotech.com...

  • Page 81: Chapter 3: -I/O Expansion Board

    Description 1-2, 3-4 Switch Brake + 5-6, 7-8 Switch Brake - Relay Only (1) default Table 3-2: -IO Option Board Fuse Information  Fuse Description Size Aerotech P/N Manufacturer's P/N +5 VDC User Power 3 A, resettable EIF01001 Raychem RGE300 www.aerotech.com Chapter 3...

  • Page 82: Analog I/O Connector (Tb201)

    Inverting Analog Input 1 Input Analog Output 1 Output Table 3-4: Mating Connector Part Numbers for the Analog Output Connector (TB201) Wire Size: AWG [mm Type Aerotech P/N Phoenix P/N 4-Pin Terminal Block ECK01293 1881341 20-28 [0.5- 0.080] Chapter 3 www.aerotech.com...

  • Page 83: Analog Output (Tb201)

    N O T E : Analog Output 0 is available on J104 (refer to Section 2.5.7.). Table 3-6: Analog Output Pins on the Analog I/O Connector (TB201) Pin# Description In/Out/Bi Analog Common Analog Output 1 Output Figure 3-2: Analog Output Connector (TB201) www.aerotech.com Chapter 3...

  • Page 84: Differential Analog Input (Tb201)

    N O T E : Analog Input 0 is available on J104 (see Section 2.5.7.). Table 3-8: Analog Input Pins on the Analog I/O Connector (TB201) Pin# Description In/Out/Bi Analog Common Non-inverting Analog Input 1 Input Inverting Analog Input 1 Input Figure 3-3: Analog Input Typical Connection (TB201) Chapter 3 www.aerotech.com...

  • Page 85: Opto Out Connectors (Digital Outputs) (Tb202/Tb203)

    It is important that the diode be installed correctly (normally reversed biased). Refer to Figure 3-6 for an example of a current sinking output with diode suppression and Figure 3-5 for an example of a current sourcing output with diode suppression. www.aerotech.com Chapter 3...
  • Page 86 Digital Output 6 (Optically-Isolated) Output Digital Output 7 (Optically-Isolated) Output Table 3-12: Mating Connector Part Numbers for the Opto Out Connectors (TB202/TB203) Wire Size: mm [AWG] Aerotech P/N Phoenix P/N 10-Pin Terminal Block ECK01294 1881406 0.5-0.080 [20-28] Chapter 3 www.aerotech.com...
  • Page 87 -IO Expansion Board Soloist CP Figure 3-4: Digital Outputs (TB202/TB203) www.aerotech.com Chapter 3...
  • Page 88 Soloist CP -IO Expansion Board Figure 3-5: Outputs Connected in Current Sourcing Mode (TB202/TB203) Figure 3-6: Outputs Connected in Current Sinking Mode (TB202/TB203) Chapter 3 www.aerotech.com...

  • Page 89: Opto In Connectors (Digital Inputs) (Tb204/Tb205)

    Digital Input 7 (Optically-Isolated) Input Internal +5 Volt Power Supply (0.5 A max) Table 3-16: Mating Connector Part Numbers for the Opto In Connector (TB204/TB205) Wire Size: mm [AWG] Aerotech P/N Phoenix P/N 10-Pin Terminal Block ECK01294 1881406 0.5-0.080 [20-28] www.aerotech.com...
  • Page 90 Soloist CP -IO Expansion Board Figure 3-7: Digital Inputs Chapter 3 www.aerotech.com...
  • Page 91 N O T E : Each bank of 8 Inputs must be connected in the all sourcing or all sinking configuration. Figure 3-8: Inputs Connected to a Current Sourcing Device Figure 3-9: Inputs Connected to a Current Sinking Device www.aerotech.com Chapter 3...

  • Page 92: User Power (Tb204, Tb205)

    User Common Connector on the Opto In Connector (TB204) Pin# Description In/Out/Bi Signal Common Table 3-18: +5 Volt Power Connector Pin on the Opto In Connector (TB205)  Pin# Description In/Out/Bi Internal +5 Volt Power Supply (0.5 A max) Chapter 3 www.aerotech.com...

  • Page 93: Relay Connector (Tb206)

    (1) For JP1 jumper configuration, refer to Table 1-1. Table 3-21: Mating Connector Part Numbers for the Relay Connector (TB206) Wire Size: AWG [mm Type Aerotech P/N Phoenix P/N 4-Pin Terminal Block ECK01293 1881341 20-28 [0.5- 0.080] The configuration of JP1...
  • Page 94 Otherwise, the user must connect J103 pin 13 to J103 pin 25. In this case, J103 would function as an interlock to prevent the Brake from releasing if the Motor Feedback connector is not connected. Figure 3-11: Brake Connected to TB206 Chapter 3 www.aerotech.com...

  • Page 95: Chapter 4: Standard Interconnection Cables

    Accessories Soloist CP Chapter 4: Standard Interconnection Cables N O T E : A complete list of Aerotech cables can be found on the website at http://www.aerotechmotioncontrol.com/manuals/index.aspx. Table 4-1: Standard Interconnection Cables Cable Part # Description Joystick Section 4.1. ECZ01231 BBA32 Interconnect Cable (1) The “-xx”...

  • Page 96: Joystick Interface

    Accessories 4.1. Joystick Interface Aerotech joysticks JI (NEMA12 (IP54) rated) and JBV are powered from 5V and have a nominal 2.5V output in the center detent position. Three buttons are used to select axis pairs and speed ranges. An optional interlock signal is used to indicate to the controller that the joystick is present.
  • Page 97 Accessories Soloist CP Figure 4-2: Two Axis Joystick Interface (to the Aux I/O of two drives) Figure 4-3: Two Axis Joystick Interface (to the Aux I/O and I/O Board) www.aerotech.com Chapter 4...
  • Page 98 Table 4-2: Cable Part Numbers Part # Cable Description UPC # C22763-XX JSXT-FLY 26HD-15DU-MAX300DM SOLOISTCP DUAL AXIS 630B2276-3 C22764-XX JSXT-26HD-15DU-MAX300DM SOLOISTCP SINGLE AXIS 630B2276-4 C22765-XX JSXT-26HD 26HD-15DU-MAX300DM SOLOISTCP DUAL AXIS 630B2276-5 C227617XX JSXT-FLY FLY-15DU-MAX300DM SOLOISTCP DUAL AXIS 630B2276-17 Chapter 4 www.aerotech.com...

  • Page 99: Handwheel Interface

    Soloist CP 4.2. Handwheel Interface A handwheel (such as the Aerotech HW-xxx-xx) can be used to manually control axis position. The handwheel must provide 5V differential quadrature signals to the Soloist CP. A handwheel can be connected to the Aux I/O as shown in...
  • Page 100 Soloist CP Accessories This page intentionally left blank. Chapter 4 www.aerotech.com...

  • Page 101: Chapter 5: Maintenance

    Turns green to indicate that the axis is in position. * If the power light flashes continuously and the unit does not operate, there is too much current draw from the 5V power supply or the control supply voltage level is low. www.aerotech.com Chapter 5...

  • Page 102: Control Board

    Soloist CP Maintenance 5.1. Control Board D A N G E R : Always disconnect the Mains power connection before opening the Soloist CP chassis. Figure 5-1: Control Board Assembly Chapter 5 www.aerotech.com...
  • Page 103 24 V operation (High Speed Input 5) 5 V operation (High Speed Input 5) 1. Default Table 5-3: Control Board Fuse Information  Fuse Description Size Aerotech P/N Manufacturer's P/N -S Option Shunt Fuse 1 A S.B. (5 mm) EIF01052 Littelfuse 215001.P -EXTSHUNT Option Shunt Fuse 2.5 A S.B.

  • Page 104: Preventative Maintenance

    The electrical power must be disconnected from the Soloist CP while cleaning. Do not allow cleaning substances or other fluids to enter the Soloist CP or to get on to any of the connectors. Avoid cleaning labels to prevent removing the label information. Chapter 5 www.aerotech.com...

  • Page 105: Appendix A: Warranty And Field Service

    Aerotech makes no warranty that its products are fit for the use or purpose to which they may be put by the buyer, whether or not such use or purpose has been disclosed to Aerotech in specifications or drawings previously or subsequently provided, or whether or not Aerotech’s...
  • Page 106 Aerotech's approval. On-site Warranty Repair If an Aerotech product cannot be made functional by telephone assistance or by sending and having the customer install replacement parts, and cannot be returned to the Aerotech service center for repair, and if Aerotech determines the problem could be warranty-related, then the following policy applies:...

  • Page 107: Appendix B: Revision History

    4.07.00 4.05.00 4.04.00 4.03.00 4.02.00 4.01.00 4.00.00 2.03.00 2.02.00 2.01.00 2.00.00 1.11a Revision changes have been archived. If you need a copy of this revision, contact Aerotech Global Technical Support. 1.11 1.10a 1.09 1.08 1.07 1.06 1.05 1.04 1.03 1.02 1.01 1.00...
  • Page 108 Soloist CP Revision History This page intentionally left blank. Appendix B www.aerotech.com...

  • Page 109: Index

    AC Line Filter 27,35 Altitude Check chassis for loose or damaged parts / Ambient Temperature hardware amplifier power dissipation Check for fluids or electrically conductive material exposure Analog Encoder Phasing Reference Diagram Cleaning Analog Encoder Specifications Continuous Output Current specifications www.aerotech.com...
  • Page 110 Inputs Connected to a Current Sinking Device Encoder Fault Interface (J207) Inputs Connected to a Current Sourcing Device 91 Encoder Fault Interface Input inspect all cables and connections Encoder Fault Interface Pin Assignment Inspect cooling vents Encoder Interface (J207) Inspection Encoder Interface Pin Assignment www.aerotech.com...
  • Page 111 Resolute absolute encoder AC Voltages RS-232 Connector Pin Assignment RS-232 Interface optional joysticks RS-232 Port Connector Mating Connector Options RS-422 Line Driver Encoder (Standard) Opto-Isolated Input Connector Pin Assignment Opto-Isolated Inputs 68,89-90 serial data stream Opto-Isolated Output Connector Pin Assignment 86 www.aerotech.com...
  • Page 112 TB106 TB201 82-84 TB204 TB205 TB206 93-94 Technical Support Thermistor Interface Thermistor Interface Input Transformer Examples Transformer Options TV0.3-28-56-ST Transformer TV0.3-56 two-axis joystick Two Axis Joystick Interface Typical Emergency Stop Circuit Typical ESTOP Interface UFM-ST unit separation unit weight www.aerotech.com...

This manual is also suitable for:

Soloist cp 10Soloist cp 20Soloist cp 30

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