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

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plz give 8085microprocessor program of equation at+bt2 ....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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import java.io.*;
class Arraysum
{
int temp;
int sum(int a,int n)
{
if(n==1)
return a;
else
{
temp =sum(a,n-1);
temp=temp+a;
return temp;
}
}
}
class Newarray
{
public static void main(String args)throws IOException
{
DataInputStream dis=new DataInputStream(System.in);
System.out.println(Enter limit);
int n=Integer.parseInt(dis.readLine());
int a=new int;
System.out.println(Enter the array);


fo ....etc

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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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sir,
i need a ppt sugesting some useful equations which would help me to find the power ratings of the motor which can be used to drive a roots type blower for pneumatic conveyor applications.I have to transport TiO2 powder to a horizontal distance of 10 m,then vertically up through 25 m and dump it in a tank there.The pipeline used is nearly 6inch in diameter. and the discharge requirements is 7200kg/hr.
Please help me...
Thanking You,
PRABHU VIJAYAN ....etc

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Yes, my organization is currently writing software analyzing ECG, your java code to find pqrst will be very helpful. Please send information to [email protected] (Hanfei Yu).

Thank you very much.

Hanfei ....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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