DocumentCode
2769021
Title
Adaptive flexible antenna array system for deformable wing surfaces
Author
Anagnostou, Dimitris ; Iskander, Mina
Author_Institution
Electr. & Comput. Eng., South Dakota Sch. of Mines & Technol., Rapid City, SD, USA
fYear
2015
fDate
7-14 March 2015
Firstpage
1
Lastpage
6
Abstract
A 4×1 coplanar and flexible antenna array for deformable surfaces is studied under different bending angles. It is assumed that the array is bent from one edge on top of an insulating cylinder (single-edge cylindrical bending). Due to flexing, the array radiates a tilted main beam. The beam can be redirected back toward its original direction by applying the correct phase difference between the elements. This compensation phase vector is calculated using a closed-form equation. Simulated results are presented, showing successful recovery of the intended radiation direction. The autonomous array can be used in unmanned aerial vehicles with wings that bend or flex on demand, morphing wings, adaptive wings, as well as on other surfaces where it is required to focus an antenna pattern toward a specific location with respect to the mounting surface.
Keywords
antenna arrays; antenna radiation patterns; adaptive flexible antenna array system; closed-form equation; compensation phase vector; correct phase difference; deformable wing surfaces; different bending angles; insulating cylinder; intended radiation direction; single edge cylindrical bending; unmanned aerial vehicles; Adaptive arrays; Antenna radiation patterns; Arrays; Mathematical model; Microcontrollers; Strain;
fLanguage
English
Publisher
ieee
Conference_Titel
Aerospace Conference, 2015 IEEE
Conference_Location
Big Sky, MT
Print_ISBN
978-1-4799-5379-0
Type
conf
DOI
10.1109/AERO.2015.7119183
Filename
7119183
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