Title
Hardware Design And Validation Of Pitching Control For Micro Air Vehicles Using Only Pressure Information
Keywords
aircraft design; micro air vehicle; pitching control; pressure sensor; wind tunnel experiment
Abstract
Micro air vehicles are small, light-weight aircraft that fly at low Reynolds numbers. They are used for information collection, especially in situations that are either hazardous for human or inaccessible for larger aerial vehicles. However, it is challenging for micro air vehicles to achieve stable flight and perform agile maneuvers in complex environments with unsteady flow. In this paper, the design and validation of pitching control for micro air vehicles using only pressure information is discussed. © 2013 AACC American Automatic Control Council.
Publication Date
9-11-2013
Publication Title
Proceedings of the American Control Conference
Number of Pages
5568-5573
Document Type
Article; Proceedings Paper
Personal Identifier
scopus
Copyright Status
Unknown
Socpus ID
84883548278 (Scopus)
Source API URL
https://api.elsevier.com/content/abstract/scopus_id/84883548278
STARS Citation
Shen, He; Xu, Yunjun; and Remeikas, Charles, "Hardware Design And Validation Of Pitching Control For Micro Air Vehicles Using Only Pressure Information" (2013). Scopus Export 2010-2014. 6238.
https://stars.library.ucf.edu/scopus2010/6238