Linearized analysis versus optimization-based nonlinear analysis for nonlinear systems
- Creators
- Topcu, Ufuk
- Packard, Andrew
Abstract
For autonomous nonlinear systems stability and input-output properties in small enough (infinitesimally small) neighborhoods of (linearly) asymptotically stable equilibrium points can be inferred from the properties of the linearized dynamics. On the other hand, generalizations of the S-procedure and sum-of-squares programming promise a framework potentially capable of generating certificates valid over quantifiable, finite size neighborhoods of the equilibrium points. However, this procedure involves multiple relaxations (unidirectional implications). Therefore, it is not obvious if the sum-of-squares programming based nonlinear analysis can return a feasible answer whenever linearization based analysis does. Here, we prove that, for a restricted but practically useful class of systems, conditions in sum-of-squares programming based region-of-attraction, reachability, and input-output gain analyses are feasible whenever linearization based analysis is conclusive. Besides the theoretical interest, such results may lead to computationally less demanding, potentially more conservative nonlinear (compared to direct use of sum-of-squares formulations) analysis tools.
Additional Information
© 2009 ACC. This work was sponsored by the Air Force Office of Scientific Research, USAF, under grant/contract number FA9550- 05-1-0266. The views and conclusions contained herein are those of the authors and should not be interpreted as necessarily representing the official policies or endorsements, either expressed or implied, of the AFOSR or the U.S. Government. U. Topcu acknowledges partial support from the Boeing Corporation. A. Packard acknowledges partial support from NASA under the contract NNX08AC80A.Attached Files
Published - Topcu2009p83662009_American_Control_Conference_Vols_1-9.pdf
Files
Name | Size | Download all |
---|---|---|
md5:b0ce51f1eefa80ef6480fc2ead979f34
|
467.5 kB | Preview Download |
Additional details
- Eprint ID
- 18250
- Resolver ID
- CaltechAUTHORS:20100512-100055574
- Air Force Office of Scientific Research (USAF)
- FA9550-05-1-0266
- Boeing Corporation
- NASA
- NNX08AC80A
- Created
-
2010-05-16Created from EPrint's datestamp field
- Updated
-
2021-11-08Created from EPrint's last_modified field