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DRIVES, MOTORS + SWITCHGEAR

T

he effect of different load inertias is illustrated with experiments

using real life components. In addition, tuning the controller is

covered in detail. Previous articles described systemtesting, servo

operating principles and a practical mechatronics case study. This article

describes the effect on the system when the load inertia is changed.

Equipment used

For the test, a brushless motor was mounted on a chassis and coupled

to a Techlyn brushless drive. Test response was measured using a

Personal Computer (PC) coupled via a serial port to the drive. Step re-

sponse was displayed while the tuning parameters were interactively

changed. Tests were carried out on the motor with no load, as well as

with flywheels dimensioned to provide load inertia of 3 X and 10 X

motor rotor inertia. Conventional wisdom states that inertia matches

of up to 10:1 are acceptable, with the optimum point being at 3:1.

Our experiments sought to see if this was indeed true. Our drive is

controlled by a Microchip PIC18F2331 microcontroller. This device is

highly optimised for motion control with all time intensive functions

being performed by hardware registers. Moves are commanded via a

serial port or step and direction digital inputs. The step and direction

inputs make the system resemble a step motor system (with encoder

position maintenance). The PC test program sends move commands

and graphs the response with respect to time.

Tests

The test motor had a rated rotor inertia of 0,23 kg.cm². Two flywheels

were machined with inertias of 0,69 kg.cm² (3:1 inertia match) and

2,3 kg.cm² (10:1 inertia match). In total, six tests were performed

and graphed.

What do the parameters on the graph mean?

Ideally, the July 2015 Electricity+Control article (Brushless servo

operating principles) should be to hand [2].

Figure 2

• On the lower left is the Servo Parameters Pane

• Kp is the Position Gain

• Kd is the Derivative Gain

• Ki is the Integral Gain

• Il is the Integration limit

• The top half shows the rotor position with respect to time

• At the lower right is the Configuration Pane which is self explana-

tory. The horizontal dotted lines are the position thresholds which

are used to measure times. The rise time for instance is the time

measured fromzero time to the first crossing of the lower threshold

PID Servo Control

These are the control filter parameters. The output to the motor

amplifier is the sum of three components:

• One, proportional to the position error providingmost of the error

correction (Kp)

• One, proportional to the rate of change in the position error which

provides a stabilising damping effect

Matching

load and servo motor sizes

Glyn Craig, Techlyn

This article, the fourth in the series, deals with stability in practical systems.

Figure1: The

mechanical part of

the test rig.

Electricity+Control

July ‘16

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