Conference proceeding
MULTI-MODEL ADAPTIVE REGULATION FOR AIRCRAFT DYNAMICS WITH DIFFERENT ZERO STRUCTURES
7TH ANNUAL DYNAMIC SYSTEMS AND CONTROL CONFERENCE, 2014, VOL 1, v 1
01 Jan 2014
Featured in Collection : UN Sustainable Development Goals @ Drexel
Abstract
An adaptive regulator is designed for parameter dependent families of systems subject to changes in the zero structure. Since continuous adaptive regulation is limited by relative degree and right half plane zeros, a multiple model adaptive regulator is implemented. The two multiple model design subproblems, covering and switching, are addressed with LQR state feedback and Lyapunov function switch logic respectively. These two subproblems are combined into a set of Linear Matrix Inequalities (LMI) and concurrently solved. The multiple model design method is applied to longitudinal aircraft dynamics.
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Details
- Title
- MULTI-MODEL ADAPTIVE REGULATION FOR AIRCRAFT DYNAMICS WITH DIFFERENT ZERO STRUCTURES
- Creators
- Eric D. Peterson - Drexel UniversityHarry G. Kwatny - Drexel UniversityASME
- Publication Details
- 7TH ANNUAL DYNAMIC SYSTEMS AND CONTROL CONFERENCE, 2014, VOL 1, v 1
- Conference
- 7TH ANNUAL DYNAMIC SYSTEMS AND CONTROL CONFERENCE, 2014, 7th
- Publisher
- Amer Soc Mechanical Engineers
- Number of pages
- 10
- Resource Type
- Conference proceeding
- Language
- English
- Academic Unit
- Mechanical Engineering and Mechanics
- Web of Science ID
- WOS:000361166500015
- Scopus ID
- 2-s2.0-84929377053
- Other Identifier
- 991019170319404721
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InCites Highlights
Data related to this publication, from InCites Benchmarking & Analytics tool:
- Web of Science research areas
- Automation & Control Systems
- Engineering, Mechanical
- Operations Research & Management Science