find an approximate solution, up to the order of epsilon

1.6k Views Asked by At

The question is to find an approximate solution, up to the order of epsilon of following problem.

$$y'' + y+\epsilon y^3 = 0$$ $$y(0) = a$$ $$y'(0) = 0$$

I tried to solve the given problem using perturbation theory.

$$y(t) = y_0(t) + \epsilon y_1(t) + \epsilon^2 y_2(t) + \cdots$$ $$t = w(\epsilon)t = (1 + \epsilon w_1 + \epsilon^2 w_2 + \cdots )t$$

However, i failed to find an appropriate approximate solution... help me!!

2

There are 2 best solutions below

0
On

You don't need a series for $t$, only $y$. So substitute $y=y_0+\epsilon y_1+\epsilon^2 y_2+\ldots$ into the equation:

$$ y_0''+\epsilon y_1''+\epsilon^2 y_2''+y_0+\epsilon y_1+\epsilon^2 y_2+\epsilon\left(y_0+\epsilon y_1+\epsilon^2 y_2\right)^3+O(\epsilon^3)=0. $$

You also have to expand the boundary conditions, which will give $y_0(0)=a$, and all other $y_i(0)=0$, and all $y_i'(0)=0$.

Now look at the equations for each magnitude of $\epsilon$. Firstly, the largest term is $O(1)$, and the equation is $$ y_0''+y_0=0 $$ so $y_0=A\sin(t)+B\cos(t)$, and the boundary condition gives $y_0=a\cos(t)$. Then the $O(\epsilon)$ equation is $$ y_1''+y_1+y_0^3=0,\ y_1(0)=y_1'(0)=0 $$ and the $O(\epsilon^2)$ equation is $$ y_2''+y_2+3y_0^2y_1=0,\ y_2(0)=y_2'(0)=0, $$ at $O(\epsilon^3)$, $$y_3''+y_3+3y_0^2y_2+3y_0y_1^2=0,\ y_3(0)=y_3'(0)=0 $$ and so on. You can solve these (remember $\cos(x)^3=3/4(\cos(3x)+3\cos(x))$) to give a series for $y$.

0
On

Following a similar problem in Question about phase shift on multiple-scale analysis, use polar coordinates in phase space $$ (y(t),y'(t))=r(t)·(\,\cos(φ(t)),\,\sin(φ(t))\,) $$ with initial conditions $r(0)=a$ and $φ(0)=0$. The unperturbed equation leads to $(y,y')=a·(\cos(-t),\sin(-t))$. Thus one expects $r(t)=a+O(ϵ)$ and $φ(t)=-t+O(ϵ)$.


From $r^2=y^2+y'^2$ one obtains $$ rr'=y'(y+y'')=-ϵy^3y'=-ϵr^4\cos^3φ\sinφ $$ or $$ \left(\frac1{r^2}\right)'=-2ϵ\cos^3 t\sin t+O(ϵ^2) $$ which integrates as $$ \frac1{r^2}-\frac1{a^2}=\fracϵ2(\cos^4t-1)+O(ϵ^2) $$ or $$ r(t)=\frac{a}{\sqrt{1-\frac12ϵa^2(1-\cos^4t)}}+O(ϵ^2) $$


From $\tan(φ)=\frac{y'}{y}$ one gets $$ φ'=\cos^2φ·\frac{y''y-y'^2}{y^2} =\frac{(y''+y)y-(y^2+y'^2)}{r^2} =-ϵr^2\cos^4φ-1\\ =-ϵa^2\cos^4t-1+O(ϵ^2) =-1 -\fracϵ8a^2(\cos4t+4\cos2t+6)+O(ϵ^2) $$ which integrates as $$ φ(t)=-t-\fracϵ{32}a^2(\sin4t+8\sin2t+24t)+O(ϵ^2) $$ which gives the correction to the average angular velocity as $-(1+\frac34ϵa^2)$