Approximate controller design for singularly perturbed aircraft systems
Graziosi, Joseph E. Sawan, M. Edwin Watkins, John Michael
Graziosi, Joseph E.
Sawan, M. Edwin
Watkins, John Michael
Citations
Altmetric:
Other Names
Location
Time Period
Advisors
Original Date
Digitization Date
Issue Date
2014-08-03
Type
Conference paper
Genre
Keywords
Aerospace control,Aircraft,Aircraft manufacture,Aircraft propulsion,Approximation methods,Atmospheric modeling,Stability analysis
Subjects (LCSH)
Citation
Graziosi, J.E.; Sawan, M.E.; Watkins, J.M., "Approximate controller design for singularly perturbed aircraft systems," Circuits and Systems (MWSCAS), 2014 IEEE 57th International Midwest Symposium on , vol., no., pp.161,164, 3-6 Aug. 2014
Abstract
The purpose of this paper is to extend the Quasi-Steady State Approximation and Matrix Block Diagonalization methods utilized in the Approximate Controller Design for Singularly Perturbed Aircraft Systems [1]. In that paper, it was shown that an approximate controller solution could be developed by relocating only the slow poles for two-time scale aircraft dynamics. In addition, it showed the difference between the approximate solutions and the exact solutions were bounded within limits as O(epsilon) and O(epsilon(2)). This technique was successfully applied to the lateral dynamics of the DeHaviland Canada DHC-2 Beaver.
Table of Contents
Description
Click on the DOI link to access the article (may not be free).
Publisher
IEEE
Journal
Book Title
Series
IEEE International Midwest Symposium on Circuits and Systems (MWSCAS)
Digital Collection
Finding Aid URL
Use and Reproduction
Archival Collection
PubMed ID
DOI
ISSN
1548-3746