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

[:=Read Full Message Here=:]

Submitted by:Isha



Introduction

Laplace's equation
Laplace's equation is a partial differential equation. Partial differential equations (PDE) are a type of differential equation, i.e., a relation involving an unknown function (or functions) of several independent variables and their partial derivatives with respect to those variables. Partial differential equations are used to formulate, and thus aid the solution of, problems involving functions of several variable ....etc

[:=Read Full Message Here=:]

//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

[:=Read Full Message Here=:]

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

[:=Read Full Message Here=:]

Hi ,Im Özge I would like to get details on simulate swing equation in simulink matlab pdf for my homework While Im searching l found this site Can you help me please ....etc

[:=Read Full Message Here=:]

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

thanks ....etc

[:=Read Full Message Here=:]

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

[:=Read Full Message Here=:]

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

[:=Read Full Message Here=:]

Plzz give a project on linear equation in two variables for class 10 ....etc

[:=Read Full Message Here=:]

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

[:=Read Full Message Here=:]