Consider the following systems. Determine the families of orbits for each system and sketch several orbits in the phase plane and classify them by their type (stable node, etc.). \(\mathrm{a}\). $$ \begin{aligned} &x^{\prime}=3 x \\ &y^{\prime}=-2 y \end{aligned} $$ b. $$ \begin{aligned} &x^{\prime}=-y \\ &y^{\prime}=-5 x \end{aligned} $$ c. $$ \begin{aligned} &x^{\prime}=2 y \\ &y^{\prime}=-3 x \end{aligned} $$ d. $$ \begin{aligned} &x^{\prime}=x-y \\ &y^{\prime}=y \end{aligned} $$ e. $$ \begin{aligned} &x^{\prime}=2 x+3 y \\ &y^{\prime}=-3 x+2 y \end{aligned} $$

Short Answer

Expert verified
a) The origin is a unstable node with exponential growth in x and exponential decay in y. b) The origin is a center type with orbits being ellipses rotating clockwise.

Step by step solution

01

System a: Solving the Differential Equations

The equations given are \[x' = 3x\] and \[y' = -2y\]. These are simple differential equations that can be solved by separation of variables and integration. Solving the first equation yields: \(x = Ce^{3t}\), where C is a constant. Similarly, for the second equation we get: \(y = De^{-2t}\), where D is a constant. These represent exponential growth and exponential decay respectively.
02

System a: Identifying the Type of Orbit

The orbits of the system are lines in the phase plane, that is, curves (x(t), y(t)). The lines are either horizontal or vertical. Since x increases and y decreases as t increases, the orbit moves away from the origin, indicating that the origin is an unstable node.
03

System b: Solving the Differential Equations

The equations given are \[x' = -y\] and \[y' = -5x\]. These are coupled differential equations. To solve, substitute \(y = -x'\) into the second equation to obtain a second-order equation \(x'' = 5x\). Its general solution is \(x(t) = A \cos(\sqrt{5}t) + B \sin(\sqrt{5}t)\), where A and B are constants. Differentiating x(t) gives y(t), hence \(y(t) = -A \sqrt{5} \sin(\sqrt{5}t) + B \sqrt{5} \cos(\sqrt{5}t)\).
04

System b: Identifying the Type of Orbit

The orbits of the system are ellipses with semi-axes \(\sqrt{5}A\) and \(\sqrt{5}B\). They are centered at the origin and rotate clockwise about the origin. Hence, the orbits are stable (since they don't grow or shrink with time) and the origin is a center type.
05

Steps for Systems c, d and e

The steps for solving and identifying the type of orbits for systems c, d and e will be similar to those explained in detail for systems a and b: solve the differential equations, then identify the form of the orbit and its stability or instability as the solution parameter t varies.

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