Laplace transforms:DC Motor circuit

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Problem

Find the steady state current i(t) through a DC motor represented by a series R-L-Motor circuit. The resistance (R) is from the armature winding. The inductance (L) is the equivalent inductance of the wire coil (which turns by current flowing through the coil in a permanent magnetic field). The motor has input current i(t) and output angular velocity ω(t). Let v(t) = 110u(t)V, R = 20Ω, L = 50mH, k = 0.05N*m/A, Jm = 0.01 kg*m2, and B = e-4N*m*s.

Solution

Since some of the elements of a motor are not typical circuit elements, we must solve this problem using Laplace transforms.

The torque is proportional to the armature current.

T(t)=ki(t)

Similarly, relating mechanical (T(t)ω(t)) and electrical (vm(t)i(t)) power, the conservation of energy requires the same proportionality between the voltage across the motor (vm(t)) and the angular velocity (ω(t)).

vm(t)=kω(t)

We want to find the Laplace transfer function of the motor, and we define it as follows.

Ω(s)=[ω(t)]/vs(s)

Summing the voltages around the series circuit gives us our differential equation.

vs(t)=Ri(t)+Ldi(t)dt+kω(t)

Take the Laplace transform.

Vs(s)=RI(s)+Ls(I(s)i(0))+kΩ(s)

At this point we can use the initial value theorem to find i(0).

i(0)=limss0i(t)estu(t)dt=e=0

Substituting i(0) into the transformed differential equation gives us Equation *1*.

Vs(s)=RI(s)+LsI(s)+kΩ(s)*1*

Repeat the process with the analogous mechanical differential equation. Here Jm is the moment of inertia of the combined armature, shaft, and load. B is the coefficient of friction.

T(t)=Jmdω(t)dt+Bω(t)

Transforming yields the following.

T(s)=Jms(Ω(s)ω(0))+BΩ(s)

Recall T(t) = k i(t), and so T(s) = k I(s). Again the initial value theorem will yield ω(0) = 0. This gives us Equation *2*.

kI(s)=(Jms+B)Ω(s)*2*

Solve Equation *2* for I(s) and substitute that into Equation *1*.

Vs(s)=(R+Ls)(Jms+B)kΩ(s)+kΩ(s)

Solve this equation for Ω(s), some simplification steps are skipped here. Equation *3*

Ω(s)=kJmLs2+(BJm+RL)s+RB+k2JmLV(s)*3*

Now in order to apply the final value theorem we let Vs(s) = K/s. The s's in the limit definition and in K/s cancel. We can now see ω in steady state.

ωss=lims0sΩ(s)=kRB+k2K=ω()

Take Equation *2* and Equation *3* and this time solve for I(s). This will get us a form of the final answer in the s domain.

I(s)=(Jms+B)k[kJmLs(s2+(BJm+RL)s+RB+k2JmL)]K=sL+BJmLs(s2+(BJm+RL)s+RB+k2JmL)K

Finally was can apply the final value theorem to see what our steady state response will be for the armature current.

iss=lims0sI(s)=BRB+k2K=i()

Answers

Of interest are the ω(∞) and i(∞), found by plugging values into the steady state solutions above.

ω()=14.91radians/second

i()=5.46Amperes



Checked by: Andrew Hellie