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Preparation of Papers in Two-Column Format - International Journal ...

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Tun<strong>in</strong>g Of PID Controller Of Inverted Pendulum Us<strong>in</strong>g Genetic Algorithm<br />

2<br />

L= ( +2 cos +<br />

2 +<br />

2 2<br />

)+ ]- cos<br />

The Euler-Lagrange’s equation for the system is given as<br />

=<br />

Us<strong>in</strong>g these two above equations we get the dynamics <strong>of</strong> the<br />

entire system<br />

……….(1)<br />

……..(2)<br />

F<br />

The system poles lies on R.H plane, hence system is<br />

unstable.<br />

Table 1. Parameters <strong>of</strong> the system from feedback<br />

<strong>in</strong>strument .U.K.<br />

Parameter Value unit<br />

Cart mass( ) 1.206 Kilo gram<br />

Mass <strong>of</strong> the<br />

pendulum( )<br />

Half Length <strong>of</strong><br />

pendulum( )<br />

Coefficient<br />

frictional force( )<br />

<strong>of</strong><br />

Pendulum damp<strong>in</strong>g<br />

coefficient(q)<br />

Moment <strong>of</strong> <strong>in</strong>ertia <strong>of</strong><br />

pendulum( )<br />

0.2693 Kilo gram<br />

0.1623 meter<br />

0.05 Ns/m<br />

0.005 /rad<br />

0.099 /<br />

Gravitation force( ) 9.8 /<br />

Fig 2 : The Inverted Pendulum System<br />

The above equation (1&2) shows the dynamics <strong>of</strong> the entire<br />

system.<br />

In order to derive the l<strong>in</strong>ear differential equation modell<strong>in</strong>g,<br />

we need to l<strong>in</strong>earaize the non l<strong>in</strong>ear differtional equation<br />

obta<strong>in</strong>ed as above so far. For small angle deviation around<br />

the upright equilibrium (fig.2) po<strong>in</strong>t assume<br />

Us<strong>in</strong>g above relation we can write as,<br />

r +q -k +d =0………..(3)<br />

…….(4)<br />

Where, ( + )= p, =k, =q, = r<br />

Eq (3&4) is the l<strong>in</strong>ear differential eqution modell<strong>in</strong>g <strong>of</strong> the<br />

entire system. In order to f<strong>in</strong>d the transfer function <strong>of</strong> the<br />

system , Laplace transform <strong>of</strong> Eq (3 & 4) has been taken out<br />

and substitut<strong>in</strong>g the parameter value (table 1), we got<br />

and<br />

IV. PERFORMANCE INDECES<br />

The design <strong>of</strong> a control system is an attempt to meet a set <strong>of</strong><br />

specifications which def<strong>in</strong>e the overall performance <strong>of</strong> the<br />

system <strong>in</strong> terms <strong>of</strong> certa<strong>in</strong> measurable quantities. In the<br />

normal way design <strong>of</strong> control system, some specific<br />

parametric values <strong>of</strong> the system are assumed and the control<br />

system is designed accord<strong>in</strong>gly to meet desired performance<br />

<strong>of</strong> the system. Here we used four most commonly<br />

mathematical functions as a performance <strong>in</strong>dex associated<br />

with error <strong>of</strong> a closed loop system. A performance <strong>in</strong>dex is a<br />

number which <strong>in</strong>dicates goodness <strong>of</strong> system performance.<br />

The objective is to design an optimal system by proper<br />

choice <strong>of</strong> its parameters such that the specified performance<br />

<strong>in</strong>dex is extremum-either m<strong>in</strong>imum or maximum. A<br />

performance <strong>in</strong>dex must be a s<strong>in</strong>gle positive number or zero,<br />

the latter be<strong>in</strong>g obta<strong>in</strong>ed if and only if the measure <strong>of</strong> the<br />

deviation becomes identically zero.<br />

The commonly used performance <strong>in</strong>deces (PI) are:<br />

Integral <strong>of</strong> squared error (ISE),<br />

J =<br />

Integral <strong>of</strong> time multiplied squared error (ITSE),<br />

J =<br />

Integral <strong>of</strong> absolute error (IAE),<br />

J =<br />

Integral <strong>of</strong> time multiplied absolute error (ITAE),<br />

J=<br />

Here the error is def<strong>in</strong>e as<br />

We have<br />

taken the stable reference model for angle whose transfer<br />

function is<br />

22

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