advertisement
Introduction Ensemble MP
Chapter 1: Introduction
Aerotech’s Ensemble MP (Ultra-Compact "Micro" PWM) network digital drive is a high performance amplifier.The drive provides deterministic behavior, auto-identification, and easy software setup. The
Ensemble MP’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.
The Ensemble MP is offered with an optional encoder interpolation feature (-MXU), an auxiliary square wave encoder input for dual loop control, dedicated analog and digital I/O (expandable with the -IO option), and separate power connections for motor and control supply voltages.
1AMP MAX
24-80VDC
TM
AEROTECH.
COM
J201
S/N -
J106
AERONET
OUTPUT
Y
OL TR
TB103
SUPPL
CON
DC-
DC+
J102
ENA
MRK
J103
CTL
1
POS
4
TB201
TB202
1
4
1
J107
AERONET
INPUT
P/N -
TB105
RS232 TX
RS232 RX
GND
WARNING:
DISCONNECT POWER
BEFORE SERVICING
TB104
DANGER!
High Voltage
ESTOP
10
TB203
1
DC+
DC-
A
B
C
80VDC MAX
10AMP MAX
10
TB204
Standard
Connector Description
J102
J103
J106
Ethernet Port
Motor Feedback
Aeronet Output
J107
TB102
TB102
TB103
TB104
TB105
Aeronet Input
Motor Supply
Motor Output
Control Supply
Emergency Stop
Sense Input (ESTOP)
RS-232
-IO Board Option
Connector Description
J201
TB201
Auxiliary Encoder
Interface
Brake Relay
TB202
TB203
TB204
Analog I/O
Opto-Inputs
Opto-Outputs
Figure 1-1: Ensemble MP Networked Digital Drive
www.aerotech.com
Chapter 1 1
Ensemble MP Introduction
Table 1-1: Feature Summary
Standard Features l l l l l l l l
Line driver square wave quadrature encoder input for position and velocity feedback
One 16-bit differential analog input (± 10 V)
Dedicated 5-24 V Emergency Stop sense input
10 - 80 VDC motor supply inputs
24 - 80 VDC control supply inputs
Calibration (refer to the Ensemble Help file for more information)
Camming (refer to the Ensemble Help file for more information)
10/100 BASE-T Ethernet port for use with Ethernet I/O modules
Options
-IO l l l l l
One 16-bit analog output (±5 V)
One 12-bit differential analog input
One fail-safe brake or user relay output
8 optically isolated logic inputs (5 - 24 VDC), may be connected in current sourcing or sinking mode
8 optically isolated logic outputs (5 - 24 VDC), user defined as current sourcing or sinking
-MXU Interpolation circuit allowing for analog sine wave input on the standard encoder channel. Interpolation factor: 4,096
Table 1-2: Accessories
Accessories
JI
PS24-1
BRAKE24-2
Industrial Joystick (NEMA12 (IP54) rated); refer to
24 VDC, 1 A power supply for optional brake/relay output
24 VDC, 2 A power supply for optional brake
External Power Supply Options
Refer to
for more information
Cables
Interconnection A complete list of Aerotech cables can be found on the website at http://www.aerotechmotioncontrol.com/manuals/index.aspx
Joystick/Handwheel Refer to
or
2 Chapter 1 www.aerotech.com
Introduction Ensemble MP
The following block diagram shows a connection summary. For detailed connection information, refer to
-IO Option
J102
Ethernet Port
J107
Aeronet Input
Encoder +5V / Common
PSO Output, Encoder Echo
SIN, COS, MRK (RS422)
J201
Secondary
Encoder
Interface
J106
TB105
RS232
TB104
ESTOP
J103
Motor
Feedback
Aeronet Output
Analog Input 1 +/-
Analog Output 1
RS232
+5V / Common
Emergency Stop Sense Input
8 Opto Outputs
(Sinking or Sourcing)
-MXU
Option
SIN, COS, MRK (RS422)
CW, CCW, Home Limits;
Encoder Fault; Hall A, B, C;
Motor Over Temperature
Brake ± (with the -IO Option)
Encoder +5V / Common
Analog Input 0 +/-
8 Opto Inputs
(Sinking or Sourcing)
TB202
TB204
Opto Out
TB203
Opto In
TB103
Control Supply
DC+
DC-
DC+
DC-
Isolated
Power Supply
Brake Power
Input or Relay
TB201
Brake
Relay
TB102
Motor
Supply
DC+
DC-
DC+
DC-
Heatsink Over
Temperature
PWM Power
Amplifier
A
B
C
A
B
C
TB102
Motor
Output
Figure 1-2: Functional Diagram
www.aerotech.com
Chapter 1 3
Ensemble MP Introduction
1.1. Drive and Software Compatibility
The following table lists the available Ensemble drives and which version of the Ensemble software first provided support for a given drive. Drives that list a specific version number in the Last Software Version column will not be supported after the listed version.
Table 1-3: Ensemble Drive and Software Compatibility
Drive Type
CL
CP
Epaq
(1)
Firmware Revision
-
A
A
B
-
A
First Software Version
1.01
2.55
1.00
2.54
1.00
2.55
Last Software Version
Current
Current
Current
Current
Current
Current
HLe
HPe
LAB
ML
MP
QDe/QL/QLe
QLAB
-
-
-
-
-
A
-
-
2.51
2.51
4.04
3.00
1.00
2.55
5.01
4.07
Current
Current
Current
Current
Current
Current
Current
Current
(1) This section does not apply to the Epaq MR. The Epaq MR contains multiple ML or MP drives. Refer to either the ML or MP drive type to determine the value for your Epaq MR.
4 Chapter 1 www.aerotech.com
Introduction Ensemble MP
1.2. Electrical Specifications
Table 1-4: Electrical Specifications
Motor Supply Input Voltage
Maximum Continuous
Input Current
Input Current
Control
Supply
Input Voltage
Input Current
Output Voltage
(1)
Refer to
MP 10
10-80 VDC
5 A rms
Section 1.2.1. System Power Requirements
24-80 VDC (±10%)
1 A max
10-80 VDC
Peak Output Current (1 second)
Continuous Output Current
Power Amplifier Bandwidth
Power Amplifier Efficiency
PWM Switching Frequency
Minimum Load Inductance
User Power Supply Output
10 A
5 A
2500 Hz maximum (software selectable)
85% - 95%
(2)
20 kHz
0.1 mH @ 80 VDC
5 VDC (@ 500 milliamps)
Modes of Operation
Protective Features
Brushless; Brush; Stepper
Output short circuit; Peak over current, DC bus over voltages; RMS over current; 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 5
Ensemble MP Introduction
1.2.1. System Power Requirements
The following equations can be used to determine total system power requirements. The actual power required from the mains supply will be the combination of actual motor power (work), motor resistance losses, and efficiency losses in the power electronics or power transformer. An EfficiencyFactor of approximately 90% should be used in the following equations.
Brushless Motor
Output Power
Rotary Motors
Linear Motors
Rotary or Linear Motors
Pout [W] = Torque [N·m] * Angular velocity[rad/sec]
Pout [W] = Force [N] * Linear velocity[m/sec]
Pout [W] = Bemf [V] * I(rms) * 3
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
6 Chapter 1 www.aerotech.com
Introduction Ensemble MP
1.2.2. Power Dissipation
The first figure below shows the amplifier power dissipation under continuous power supply and output current conditions. The values on the graph represent the peak current that the amplifier would provide during operation. When the bus voltage and output current are known, the amplifier power dissipation is found using this graph. The second figure shows the maximum recommended ambient temperature as a function of amplifier power dissipation. Use this graph along with the power dissipation obtained from the first graph to determine the maximum ambient temperature. If the result is lower than the known operating ambient temperature, additional measures are required to cool the Ensemble MP. Mounting it to a large metal plate for extra heat-sinking and providing additional fan flow are suggested.
18
16
14
12
10
8
6
4
2
0
0
80V Bus
40V Bus
0.6
1.2
1.8
2.4
3
Output Current (A)
3.6
4.2
Figure 1-3: Power Dissipation vs. Output Current
4.8
120
100
80
60
40
20
0
0
Absolute Maximum
Recommended
2 4 6 8 10
Amplifier Dissipation (W)
12 14 16
Figure 1-4: Ambient Temperature vs. Power Dissipation
EXAMPLE:
80 VDC Bus operation at 2.4 A
Power Dissipation = 7.5 Watts
Maximum Ambient Temperature = 53°C www.aerotech.com
Chapter 1 7
Ensemble MP Introduction
1.3. Mechanical Design
Install the unit into a construction compliant for unlimited circuits enclosure. Each unit should be separated from other drives and surrounded by 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.
7.6 [0.30]
41.1 [1.62]
25.4 [1.00]
DIMENSIONS: MM [INCH]
Dimensions apply to the standard and I/O version (shown) of the MP drive.
TM
AEROTECH.
COM
J201
J102
ENA
MRK
CTL
POS
1
4
TB201
TB202
1
4
1
J103
10
TB203
1
DC+
DC-
A
B
C
80VDC MAX
10AMP MAX
10
TB204
4.0 [0.16] (TYP.)
REC. MTG. HDWR: M3.5 [#6]
Figure 1-5: Dimensions
Table 1-5: Physical Specifications
Standard w/ -IO option w/ -MXH option
Weight
0.454 kg (1.0 lb)
0.544 kg (1.2 lb)
0.544 kg (1.2 lb)
107.0 [4.21]
121.4 [4.78]
Typical Size 100 mm x 125 mm x 2.4 mm (4 in x 5 in x 0.094 in)
Drawing Number: 630D2077
2.5 [0.10]
8 Chapter 1 www.aerotech.com
Introduction Ensemble MP
1.4. Environmental Specifications
The environmental specifications for the Ensemble MP are listed below.
Ambient Temperature Operating: 0° to 50°C (32° to 122° F)
Storage: -30° to 85°C (-22° to 185° F)
Humidity
Altitude
Maximum relative humidity is 80% for temperatures up to 31°C. Decreasing linearly to 50% relative humidity at 40°C. Non condensing.
Up to 2000 meters.
Pollution
Use
Pollution degree 2 (normally only non-conductive pollution).
Indoor use only.
www.aerotech.com
Chapter 1 9
Ensemble MP Introduction
This page intentionally left blank.
10 Chapter 1 www.aerotech.com
advertisement
* Your assessment is very important for improving the workof artificial intelligence, which forms the content of this project
Related manuals
advertisement
Table of contents
- 1 Ensemble MP Hardware Manual
- 3 Table of Contents
- 5 List of Figures
- 7 List of Tables
- 9 EC Declaration of Conformity
- 10 Agency Approvals
- 11 Safety Procedures and Warnings
- 13 Quick Installation Guide
- 15 Chapter 1: Introduction
- 18 1.1. Drive and Software Compatibility
- 19 1.2. Electrical Specifications
- 20 1.2.1. System Power Requirements
- 21 1.2.2. Power Dissipation
- 22 1.3. Mechanical Design
- 23 1.4. Environmental Specifications
- 25 Chapter 2: Installation and Configuration
- 25 2.1. Power Connections
- 26 2.1.1. Control Supply Connections (TB103)
- 27 2.1.2. Motor Supply Connections (TB102)
- 28 2.1.3. External Power Supply Options
- 30 2.1.4. Minimizing Conducted, Radiated, and System Noise
- 31 2.2. Motor Output Connections
- 32 2.2.1. Brushless Motor Connections
- 33 2.2.1.1. Powered Motor Phasing
- 35 2.2.1.2. Unpowered Motor and Feedback Phasing
- 38 2.2.2. DC Brush Motor Connections
- 39 2.2.2.1. DC Brush Motor Phasing
- 40 2.2.3. Stepper Motor Connections
- 41 2.2.3.1. Stepper Motor Phasing
- 42 2.3. Motor Feedback Connections (J103)
- 43 2.3.1. Encoder Interface (J103)
- 44 2.3.1.1. RS-422 Line Driver Encoder (Standard)
- 45 2.3.1.2. Analog Encoder Interface
- 47 2.3.1.3. Encoder Phasing
- 49 2.3.2. Hall-Effect Interface (J103)
- 50 2.3.3. Thermistor Interface (J103)
- 51 2.3.4. Encoder Fault Interface (J103)
- 52 2.3.5. End Of Travel Limit Input Interface (J103)
- 54 2.3.5.1. End Of Travel Limit Phasing
- 55 2.3.6. Brake Output (J103)
- 56 2.3.7. Analog Input 0 (J103)
- 57 2.4. Emergency Stop Sense Input (TB104)
- 58 2.4.1. Typical ESTOP Interface
- 59 2.5. Aeronet Interface (J106/J107)
- 60 2.6. RS-232 Interface (TB105)
- 61 2.7. PC Configuration and Operation Information
- 63 Chapter 3: -I/O Expansion Board
- 64 3.1. User Power (TB201)
- 65 3.2. Brake Power Supply (TB201)
- 68 3.2.1. Solid State Relay Specifications (TB201)
- 69 3.3. Analog Output (TB202)
- 70 3.4. Analog Input (TB202)
- 71 3.5. Opto-Isolated Inputs (TB203)
- 74 3.6. Opto-Isolated Outputs (TB204)
- 78 3.7. Auxiliary Encoder Channel/PSO Output (J201)
- 80 3.7.1. Position Synchronized Output (PSO)/Laser Firing (J201)
- 83 Chapter 4: Standard Interconnection Cables
- 84 4.1. Joystick Interface
- 86 4.2. Handwheel Interface
- 87 Chapter 5: Maintenance
- 88 5.1. Control Board
- 90 5.2. Preventative Maintenance
- 91 Appendix A: Warranty and Field Service
- 93 Appendix B: Revision History
- 95 Index