Novel design and optimization of S band patch antenna for space application by using a gravitational search algorithm

The design of the patch antenna oriented for space application is a balanced solution between multiple disciplines. New disciplines are considered in these studies such as vibration and cost. To address the challenges, a novel framework called Multidisciplinary Design Optimization is developed inclu...

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Bibliographic Details
Published in:International journal on interactive design and manufacturing 2023-06, Vol.17 (3), p.1131-1148
Main Authors: Zafrane, Mohammed Amine, Mebrek, Mohammed Ali, Souillah, Hadjer, Madouri, Zineb Bouchra, Abes, Bachir
Format: Article
Language:English
Subjects:
Algorithms
Antennas
CAE) and Design
Composite materials
Computer-Aided Engineering (CAD
Configuration management
Design optimization
Electronics and Microelectronics
Engineering
Engineering Design
Geometry
Industrial Design
Instrumentation
Mechanical Engineering
Microsatellites
Monte Carlo simulation
Multidisciplinary design optimization
Original Paper
Parameters
Patch antennas
Satellites
Search algorithms
Software
Substrates
Superhigh frequencies
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Summary:The design of the patch antenna oriented for space application is a balanced solution between multiple disciplines. New disciplines are considered in these studies such as vibration and cost. To address the challenges, a novel framework called Multidisciplinary Design Optimization is developed including problem definition, multidisciplinary modeling and a heuristic optimizer. The Gravitational Search algorithm is used to enhance the performance parameters of the proposed configuration. The performance parameters are computed at the resonating frequencies of the proposed antenna. Two polarized configurations in S-band are proposed: rectangular and circular. A proof-of-concept design example is the 2.4 GHz patch antenna using Rogers substrate material which has demonstrated the effectiveness of the proposed framework. The proposed antenna could be a successful choice for micro satellite applications.
ISSN:1955-2513
1955-2505
DOI:10.1007/s12008-022-01074-x