INFORMATION AND CONTROL ENGINEERING LABORATORY

16.338: NONLINEAR AEROSPACE CONTROL SYSTEMS

DESCRIPTION
This course is an introduction to nonlinear dynamical systems. It aims at providing both theoretical and experimental knowledge of nonlinear dynamical systems.

On the theory side, we'll study ordinary differential equations and how to simulate them. We'll describe back-of-the envelope techniques to study second-order systems, like phase-plane control system analysis and synthesis. We'll see qualitative properties of several nonlinearities, like deadband, saturation, dry friction, backlash. Several applications of nonlinearities will be investigated, like pulse modulation systems, nonlinear integrators with limited phase loss and others. Notions of bifurcation theory will be explained at the elementary level, including frequency response jumps. Describing functions will be introduced as a convenient yet heuristic way to investigate nonlinear systems. We will introduce non-heuristic analysis methods based on Lyapunov's stability theory and their computer implementation.

During the experimental part of this course, you will operate a wind tunnel to investigate aerodynamic nonlinearities, transform a sabre saw into an open-loop, stable inverted pendulum, build a bowlfeeder and/or operate nonlinear flexible structures.

Prof. Feron operating a triply inverted, open-loop stable pendulum in the basement of Bdg 33. Hard to believe, but there are no springs at the hinges and these are frictionless!
Blunt bodies such as square sections sometimes exhibit negative lift. This pendulum, operated in the 1' wind tunnel in the basement of Bdg 33, exhibits interesting limit cycling properties.
PREREQUISITES
16.060, 16.31, 6.302 or 2.003
WHEN AND WHERE
TBD
CONTACT
Professor Eric Feron
Room 33-217
3-1991
FRONT PAGE * AERO/ASTRO * MIT * FEEDBACK
edited by mlcar@mit.edu on May 12, 1998