[] System Decoupling By Design; Application to Tensegrity Structures

Jan 15

Thursday, January 15, 2015

11:30 am - 1:00 pm

Presenter

Dr. Cornel Sultan, Virginia Tech

Coordinate coupling raises serious numerical, analysis, and control design problems that grow with the size of the system. On the other hand, decoupled dynamic equations facilitate numerical computation, analysis, control design since each equation can be treated independently. Unfortunately, most practical, complex systems, are not naturally decoupled so developing accurate enough decoupled approximations is of interest. 

In this talk the issue of building such accurate decoupled approximations for second order systems is addressed by leveraging concepts from robust control theory. For this purpose, first a parameter dependent decoupled approximation model is constructed for an original system that is coupled. System gains (e.g. energy gain, peak to peak gain) are used to characterize the approximation error between time responses of the coupled system and its decoupled approximation. A key advantage of system gains is that they characterize the approximation error in time domain over large classes of physically and theoretically relevant signals (e.g. finite energy/finite peak signals). Then some system parameters (e.g. damping, stiffness coefficients) are selected using stochastic optimization to design the original system such that the approximation error is minimized. Effectively, the physical system is designed to provide a decoupled approximation model that guarantees accurate approximation for an entire class of signals. This is a major advantage for many practical applications when perturbation signals can be described only in terms of limited features.

Since these ideas originated from a long standing interest of the presenter in research in structural dynamics and control, examples that use tensegrity structures are included. These structures are designed to yield accurate decoupled linear models with respect to all signals of finite energy and finite peak. Further analysis corrects several misconceptions regarding decoupling, system properties, and control design.

Cornel Sultan holds a Ph.D. in Aerospace Engineering from Purdue University, a M.S. in Mathematics, and a B.S./M.S. in Aerospace Engineering from Bucharest Polytechnic University (Romania). He has been affiliated, among others, with Harvard Medical School, where he worked on mathematical modeling of cells, and United Technologies Research Center, where he led projects on helicopter modeling and control. Currently he is an Associate Prof. in the Aerospace and Ocean Engineering Department at Virginia Tech where his principal research activities are in the modeling, control and design of tensegrity structures, membranes, helicopters, and energy harvesting systems. He received a NSF CAREER Award in 2010.

Contact

Michele Thompson
919-660-5336
mthomp@duke.edu