DIRECT ADAPTIVE CONTROL OF NONLINEAR SYSTEMS WITH UNCERTAIN UNSTABLE ZERO DYNAMICS
Abstract
The proposed research focuses on a fundamental and challenging problem in feedback control theory with well-documented applicability to a pressing need in advanced aerospace technology. In particular, the theoretical thrust of this research is aimed at the problem of controlling systems with uncertain unstable zero dynamics. Systems with these properties are extremely challenging, and no existing methods are able to address them with any level of reliability. At the same time, this research is timely since it is directly motivated by the dynamics of hypersonic vehicles. This need is well documented in the literature and highlighted by ight experiments.
Document Details
- Document Type
- DoD Grant Award
- Publication Date
- Aug 12, 2021
- Source ID
- FA95502010028
Entities
People
- Dennis S. Bernstein
Organizations
- Air Force Office of Scientific Research
- Board of Regents of the University of Michigan
- United States Air Force