hello please can any one give one example tabu search code ..i understood concept but i want to see one example

thanks..............etc

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progaram for Three Colour Display Using Bicolor Led ??????????..............etc

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TEMPERATURE CONTROLLER USING 8085 MICROPROCESSOR



PROJECT DESCRIPTION:
Industrial and control application/may require automation of the process such as temperature, pressure, liquid flow, etc., in order to minimize manual intervention. To automate any application an intelligent processor plays a major role. One such processor proposed for the project is 8085, an 8-bit microprocessor.
The temperature controller can be used to control the temperature of any..............etc

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hello please can any one give one example tabu search code in matlab ..i understood concept but i want to see one example

thanks..............etc

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I am Shakti, I would like to what is the program to find the roots of quadratic equation in a 8085 microprocessor...............etc

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plz give 8085microprocessor program of equation at+bt2..............etc

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seminar on quadratic equation for 10 class
..............etc

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hi
I'm doing my 2yr B.tech IT, I have a mini project on the

Title:Temperature Controller using microprocessor 8085 or 8086

I need these contents :
abstract, introduction,hardware required, working principle, procedure, an assembly language program , conclusion


If u have any idea or any information.... please reply me
Thank You ..............etc

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//QuadEqn.java
package p;
interface Quadratic
{
void process();
}
public class QuadEqn implements Quadratic
{
double a,b,c,d;
public QuadEqn(double x,double y,double z)
{
a=x;
b=y;
c=z;
}
public void process()
{

d=b*b-(4*a*c);
if(d==0)
{
double r=-b/2*a;
System.out.println(Roots are equal.Root=\t+r);
}
else
if(d>0)
{
double sq=Math.sqrt(d);
double r1=(-b+sq)/2*a;
double r2=(-b-sq)/2*a;
System.out.println(Root1=\t+r1+\nRoot2=\t+r2);
}
else
System.out.pri..............etc

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Presented By:-
Tejaswinee Darure


Longitudinal Dynamics
u(t) : axial velocity
w(t) : normal velocity
V(t) : velocity magnitude
α(t) : angle of attack
γ (t) : flight path angle
θ (t) : pitch angle
 x’(t) = Ax(t) + Bu(t) --------(1)
Consider , state feedback as -
u(t)= - K*x(t) --------(control law)
 This indicates that instantaneous states are given as feedback where ..............etc

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