CDS 140a Winter 2015 Homework 8
R. Murray | Issued: 23 Feb 2015 |
CDS 140, Winter 2015 | Due: 4 Mar 2015 at 12:30 pm In class or to box across 107 STL |
- Perko, Section 4.4, Problem 1a Show that for $a + b \neq 0$ the system
<amsmath> \aligned \dot x &= \mu x - y + a (x^2 + y^2) x - b (x^2 + y^2) y + O(|x|^4) \\ \dot y &= x + \mu y + a (x^2 + y^2) x + b (x^2 + y^2) y + O(|x|^4) \endaligned
</amsmath>has a Hopf bifurcaton at the origin at the bifurcation value $\mu = 0$. Determine whether it is supercritical or subcritical.
- Perko, Seciton 4.4, Problem 2
Consider the $C^1$ system
<amsmath> \aligned \dot x &= \mu x - y - x \sqrt{x^2 + y^2} \\ \dot y &= x + \mu y - y \sqrt{x^2 + y^2} \endaligned
</amsmath>(a) Show that the vector field $f$ defined this system belongs to $C^1({\mathbb R}^2 \times {\mathbb R})$: i.e.. show that all of the first partial derivatives with respect to $x$, $y$ and $\mu$ are continuous for all $x$, $y$ and $\mu$
(b) Write this system in polar coordinates and show that for $\mu > 0$ there is a stable limit cycle around the origin aucl that for $\mu < 0$ there is no limit cvcle around the origin. Sketch the phase portraits fur these two cases.
(c) Sketch the bifurcation diagram for the system, making sure that the size of the limit cycle as a function of $\mu$ is accurately represented.
- The Moore-Greitzer equations model rotating stall and surge in gas turbine engines describe the dynamics of a compression system, such as those in gas turbine engines. The three-state "MG3" equations have the form:
<amsmath> \aligned \frac{d\psi}{dt} &= \frac{1}{4 B^2 l_c}\left(\phi - \Phi_T(\psi) \right), \\ \frac{d\phi}{dt} &= \frac{1}{l_c}\left( \Psi_c(\phi) - \psi + \frac{J}{8} \frac{\partial^2 \Psi_c}{\partial \phi^2} \right), \\ \frac{dJ}{dt} &= \frac{2}{\mu + m} \left( \frac{\partial \Psi_c}{\partial \phi} + \frac{J}{8} \frac{\partial^3 \Psi_c}{\partial \phi^3} \right) J, \endaligned
</amsmath>where <amsmath>\psi</amsmath> represents the pressure rise across the compressor, <amsmath>\phi</amsmath> represents the mass flow through the compressor and <amsmath>J</amsmath> represents the amplitude squared of the first modal flow perturbation (corresponding to a "rotating stall" disturbance). For the Caltech compressor rig, the parameters and characteristic curves are given by:
<amsmath> \aligned B &= 2, & \Phi_T(\psi) &= \gamma \sqrt{\psi},\\ l_c &= 6, & \Psi_c(\phi) &= 1 + 1.5 (\phi-1) - 0.5 (\phi-1)^3, \\ \mu &= 1.25, &\qquad\qquad m &= 2. \endaligned
</amsmath>The parameter <amsmath>\gamma</amsmath> represents the throttle setting and typically varies between 1 and 2.
(a) Compute the bifurcation diagram for the system showing the equilibrium value(s) for <amsmath>J</amsmath> as a function of <amsmath>\gamma</amsmath>. Your answer should match what was shown in class (i.e., make sure to get capture the hysteresis loop).
(b) Suppose that we can modulate the throttle, so that <amsmath>\gamma = \gamma_0 + u</amsmath>. Analyze the performance of the system using the Liaw-Abed control law <amsmath>u = k J</amsmath>. Show that if we choose <amsmath>k</amsmath> sufficiently large we can cause the bifurcation to stall to be supercritical.
(c) Suppose that we restrict the dynamics of the system to the invariant set given by $J = 0$. Show that the system undergoes a subcritical Hopf bifurcation (this phenomena is called "surge").