**Documentation Home Page** ◇ **Courseware Home Page**

Pour la **documentation en FRANÇAIS**, utilisez l'outil de traduction de votre navigateur Chrome, Edge ou Safari. Voir un exemple.

# DCM - Introduction

# Page Content

The diagram of the virtual laboratory test bench is shown in figure 1.

**Figure 1**: Virtual Test Bench of the DCM Drive

The major elements in the test bench are:

- The DC motor under test (
**MUT**) with adjustable field voltage*Vf*. - A DC machine with adjustable field voltage and a variable load.
- Command switches (
**K1**) and (**K2**) allow connecting the MUT and DCM to the single-phase two-level inverter, while (**K3**) allows the connection (disconnection) of the variable load to (from) DCM. - A mechanical shaft coupling the DCM and MUT.
- A protection system composed of fuses connected in series with the windings from both machines.
- A single-phase two-level inverter as armature voltage to either the MUT or the DCM.

The different modules covered in this laboratory are discussed next.

# DC Motor Parameters Identification

## Determination of the back-emf Constant *Ke*

The back electromotive force (emf) that is generated in a DC motor is directly proportional to the speed ω of the motor **[2]**.

To determine *Ke*, the MUT is driven at a certain speed by the DC machine running as a motor (see figure 2).

During this test, switch (**K1**) is closed, and the MUT armature voltage is open.

**Figure 2**: Open Circuit Test for the Determination of Ke

By varying the applied voltage, different switching pulses are generated to drive the inverter, which then applies different voltages to the DCM armature.

This leads to the DCM driving the MUT at different speeds that are recorded, while at the same time measuring the open circuit armature voltage *Va*.

The student can then plot the speeds and the measured Va values and find the slope of this line.

This slope corresponds to *Ke* as seen from equation **(1)** above.

## Determination of the Armature Resistance *Ra*

To estimate the MUT armature resistance, a varying voltage is applied to its armature via the inverter.

The MUT drives the DCM running as a generator which is connected or not to a variable load resistance (see figure 3).

The armature voltage of the MUT can be written as:

Under the assumption of steady state, equation (2) is rewritten as:

**Figure 3**: Steady State Test for the Determination of Ra

From **(3)**, *Ra* is obtained as:

With *Ke* known, one can determine *Ra* by measuring the armature voltage *Va* and current Ia of the MUT, and its speed ω (referred to as *N* in figure 3) for a random operating point.

For a more accurate result, the student can test many different operating points, and then take the average result as an estimation of the armature resistance.

## Determination of the Armature Inductance *La*

**Figure 4**: Blocked Rotor Test for the Determination of La

To estimate the armature inductance, the motor under test must be held in a standstill, ω = 0 (locked rotor), as shown in figure 4.

Therefore, equation **(2)** above simplifies to:

At time (right after a step voltage is applied), the instantaneous current is so we can say from the voltage equation in (5) that:

From (6), one can determine the value of *La* by measuring *Va* during the block rotor test and the slope of the armature current right after the step voltage is applied.

It is important to mention that during the blocked rotor test, the applied voltage should not exceed 10% of the MUT nominal voltage.

Note

The parameters *Ke*, *Ra*, and *La* are defined as the **electrical parameters** of the brushed-DC motor under test.

## Determination of the Friction Torque Tf and Friction Coefficient *B*

**Figure 5**: Identification of Friction Parameters

The equation for the electrical torque in steady state (constant speed) can be approximated by a friction-type model** [2, 3]**:

where is the MUT electromagnetic torque [Nm] and is the load torque applied on the shaft [Nm].

In a no-load test, there is no load torque and the expression simplifies to:

To simulate the no-load test, the MUT drives the DCM running as a generator with switch **K3** open (see figure 5 above).

The student can apply different voltage values and record the speed and armature current of the MUT.

With the armature current known, the electromagnetic torque can be calculated as:

Finally, plot the values of speed (x-axis) vs *Te* and find the slope of the line and the y-intercept.

The slope corresponds to the friction coefficient *B*, and the y-intercept to the friction torque* Tf*.

## Determination of the Moment of Inertia *J*

**Figure 6**: Identification of the Moment of Inertia

The equation for the electrical torque in transient state (acceleration or deceleration) is as follows:

If the motor is instantly shut off from steady state and there is no applied load torque, we obtain:

Where is the speed [rad/s] at shutoff time .

From this, we can isolate the moment of inertia:

As shown in figure 6 above, the MUT is mechanically coupled to the DC machine acting as a generator for the determination of the inertia *J*.

With switch **K2** closed, the model runs until steady state is reached, then the motor is shut off.

A plot of decreasing motor speed is obtained from this operation.

To find the inertia, equation (12) is used by considering two points at the very beginning of the decreasing slope.

The current is the armature current at the shutoff time , while is equal to the back-emf constant Ke (see equation **(9)** above).

Note

The parameters , *B*, and J are defined as the **mechanical parameters** of the brushed-DC motor under test.

# DC Motor Current Control

The first and simplest way to control a DC motor is with a current control loop (see figure 7).

This is because in a DC motor, the torque and the current have a purely linear relationship.

The objective is to output a voltage that can achieve a current in the machine that matches the input reference current.

A simple proportional-integral (PI) controller can then be designed for the current of the DC motor.

Such a controller has a transfer function of the following form (note that for simplicity, the equations are shown in the Laplace domain, but know that in this laboratory they are implemented in the discrete domain as it is a requirement for real-time simulation):

**Figure 7**: Closed-Loop Current Control

There are multiple methods to calculate proper values for the gain constants and .

One method is to analyze the transfer function of the electrical model of the DC motor:

Since there is a pole at in the motor transfer function, we select the gain constants such as to cancel out this pole in the overall transfer function:

This can be done by enforcing the condition:

Performing this cancellation and manipulating the system’s transfer function allows for the following relationships for the gain constants to be found:

where is the selected crossover frequency in rad/s.

For best performance, we select this value to be about two orders of magnitude smaller than the switching frequency of the PWM carrier signal because we wish to avoid interference in the loop from noise in the switching frequency (in our case =1980 Hz, so we could approximately choose =20 Hz).

Note

The parameter V_{DC} is the input DC voltage of the single-phase two-level inverter, and its value is 460 V.

More details are provided later about the parameters and ratings of the different test bench components.

# DC Motor Speed Control

The idea for speed control is similar to current control, except that the input to the control loop is the reference speed N*.

The output of the speed controller yields a torque reference T* which is multiplied by a gain *K* to become the reference input current to the current PI controller (see figure 8).

In other words, the speed control forms the outer loop and current control is the inner loop of the overall system.

The actual machine speed is fed back into the PI speed regulator to correct for errors.

**Figure 8**: Closed-Loop Speed Control

Note

The gain *K* is the inverse of the back-emf constant: *K* = 1/K_{e}.

OPAL-RT TECHNOLOGIES, Inc. | 1751, rue Richardson, bureau 1060 | Montréal, Québec Canada H3K 1G6 | opal-rt.com | +1 514-935-2323

Follow OPAL-RT: LinkedIn | Facebook | YouTube | X/Twitter