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Control azimut antena, Exámenes selectividad de Mecánica

Modelo matemático para el control de posición de una antena de azimut

Tipo: Exámenes selectividad

2020/2021

Subido el 24/03/2022

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Analysis of an electromechanical system
Final Exam
Ivan Mauricio Melo Melo
Estudiante de Ingeniería Mecatrónica
Universidad Autónoma de Occidente
Cali, Colombia
ivan.melo@uao.edu.co - 2196155
In summary, this document includes the
mathematical model of an
electromechanical system that consists of
the displacement of an antenna, with a
position input, with the mathematical
model the transfer function is found, which
allows graphing the system to observe the
responses to a step entrance.
The position control system transforms the
position input signal into an output
response, also position, the position
control is found in many systems, such as
antennas, robotic arms, computer disk
drives, Among many more, in figure 1, an
example of them can be observed, which is
a system in which it has an azimuth output
that follows an input angle given by a
potentiometer, the latter converts said
angular displacement into a voltage, in the
same way the other potentiometer works
the same, and has a dc motor, a differential
amplifier and a power amplifier, and of
course, a load on the rotor.
Figure 1. Antenna system - layout.
Figure 2. Antenna system - schematic.
First, the mathematical model of the
engine is proposed:
𝑅𝑎𝐼𝑎+ 𝐿𝐼󰇗𝑎+ 𝑉 = 𝑒𝑎 [1]
𝑉 = 𝐾𝑏𝜃󰇗𝑚 [2]
𝑇𝑚= 𝐾𝑡𝐼𝑎 [3]
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Analysis of an electromechanical system

Final Exam

Ivan Mauricio Melo Melo

Estudiante de Ingeniería Mecatrónica

Universidad Autónoma de Occidente

Cali, Colombia

[email protected] - 2196155

In summary, this document includes the

mathematical model of an

electromechanical system that consists of

the displacement of an antenna, with a

position input, with the mathematical

model the transfer function is found, which

allows graphing the system to observe the

responses to a step entrance.

The position control system transforms the

position input signal into an output

response, also position, the position

control is found in many systems, such as

antennas, robotic arms, computer disk

drives, Among many more, in figure 1, an

example of them can be observed, which is

a system in which it has an azimuth output

that follows an input angle given by a

potentiometer, the latter converts said

angular displacement into a voltage, in the

same way the other potentiometer works

the same, and has a dc motor, a differential

amplifier and a power amplifier, and of

course, a load on the rotor.

Figure 1. Antenna system - layout.

Figure 2. Antenna system - schematic.

First, the mathematical model of the

engine is proposed:

𝑎

𝑎

𝑎

𝑎

[1]

𝑏

𝑚

[2]

𝑚

𝑡

𝑎

[3]

The previous equations are passed to

Laplace, giving as a result:

𝑎

𝑎

𝑎

𝑎

(𝑠) [1*]

𝑏

𝑚

(𝑠) [2*]

𝑎

𝑇

𝑚

(𝑠)

𝐾

𝑡

[3*]

We replace 3 * and 2 * in 1 *, giving an

equation such that:

( 𝑅

𝑎

+𝐿

𝑎

𝑆

) 𝑇

𝑚

( 𝑠

)

𝐾 𝑡

𝑏

𝑚

𝑎

(𝑠) [4]

Figure 3. Torque Tm.

With figure 3, the following equation is

obtained, which corresponds to the torque

𝑚

𝑚

𝑚

2

𝑚

𝑚

[5]

With equations 4 and 5, and considering

that L = 0, the transfer function of input

𝑎

and output 𝜃

𝑚

can be found:

𝑎

𝑡

𝑚

𝑚

𝑏

𝑚

𝑎

𝑎

𝑚

𝑎

𝑚

𝑎

𝑚

2

𝑚

𝑎

𝑏

𝑡

𝑡

𝑚

𝑎

2

𝑚

𝑚

𝑏

𝑡

𝑎

𝑡

𝑎

𝑚

𝑚

𝑎

𝜃

𝑚

( 𝑠

)

𝑒 𝑎

( 𝑠

)

𝐾

𝑡

𝑅 𝑎

𝐽 𝑚

𝑆[𝑆+

1

𝐽

𝑚

(𝐷

𝑚

𝐾

𝑏

𝐾

𝑡

𝑅

𝑎

)]

𝐾

𝑚

𝑆(𝑆+𝑎 𝑚

)

[6]

Equation 6 is the relationship between the

motor and the load.

Figure 4. Motor - torque relationship.

Considering that the equivalent inertia 𝐽

𝑚

and the equivalent viscous damping 𝐷

𝑚

as we see in figure 4, are given by:

𝑚

𝑎

𝑁

1

𝑁

2

2

𝐿

[7]

𝑚

𝑎

𝑁 1

𝑁

2

2

𝐿

[8]

Now, for the potentiometers, since the

input and output of the potentiometers are

configured in the same way, the transfer

functions of both will be the same, they are

represented by a relationship between the

voltage output and the angular positioning

input, the which is proportional:

𝑉 𝑖

(𝑠)

𝜃

𝑖

(𝑠)

𝑉

𝑁∗𝜋

𝑝𝑜𝑡

[9]

Now, we have the preamplifier, which

shows the transfer function when we have

the input 𝑉

𝑒

(𝑠), to obtain an output

𝑝

𝑉

𝑝

(𝑠)

𝑉 𝑒

( 𝑠

)

= 𝐾 [10]

In the introduction of the system, the

observation is made that:

𝑉

2 𝜋

[10*]

Figure 6. Response to a step.

In figure 6, the response of the transfer

function obtained in the development of

the system can be observed, with a given

step, which is reflected in the output by

means of a graph.

Figure 7. Map poles and zeros.

In figure 7 is the map of poles and zeros,

from which it can be induced, which will

have a slow response, since the pole is

very close to the origin, and this makes it

have a later response, as shown you can

see in the step response. On the other

hand, as it has no real part, no oscillations

will be observed.

Figure 8. Bode diagram.

In figure 8, you can see the graph which

shows us the magnitude in dB and the

phase in Deg, in relation to the frequency

given by Rad / s, also known as the bode

diagram.

Figure 9. Frequency for - 20dB

attenuation.

In figure 9, it was obtained from figure 8,

in which a frequency in which it has a

magnitude of - 20dB was searched, which

attenuates the system.

Figure 10. Transitory and stationary

regime.

In figure 10, we can see the representation

of the transitory and the stationary regime

which correspond, the transitory regime is

the space of time in which the function is

not in a constant response, but on the

contrary, it is varying, and consequently,

the stationary regime is when the signal is

at a constant which does not vary with

respect to the y-axis.

To conclude the analysis of this system,

the opportunity was given to use software

such as Matlab's, the feedback from some

other book recommended by the teacher,

in which they explain in a concrete way

the equations necessary to carry out the

exercise, on the other hand On the other

hand, it was possible to observe the

response of a position control system

which had not had the time to work with

one, the development of the system and

its respective analyzes became very

enjoyable.

References:

[1] Norman S, Nise - Control Systems

Engineering.