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
Link To Document :
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