Antenna Model with Pattern Optimization Based on Genetic Algorithm for Satellite-Based SAR Mission

Synthetic aperture radar (SAR) systems are of paramount importance to remote sensing applications, including Earth observation and environmental monitoring. Accurate calibration of these systems is imperative to ensuring the accuracy and reliability of the acquired data. A central component of the c...

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Published inSensors (Basel, Switzerland) Vol. 25; no. 15; p. 4835
Main Authors Sánchez-Sevilleja, Saray, García-Rodríguez, Marcos, Masa-Campos, José Luis, Cuerda-Muñoz, Juan Manuel
Format Journal Article
LanguageEnglish
Published Switzerland MDPI AG 06.08.2025
MDPI
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ISSN1424-8220
1424-8220
DOI10.3390/s25154835

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Summary:Synthetic aperture radar (SAR) systems are of paramount importance to remote sensing applications, including Earth observation and environmental monitoring. Accurate calibration of these systems is imperative to ensuring the accuracy and reliability of the acquired data. A central component of the calibration process is the antenna model, which serves as a fundamental reference for characterizing the radiation pattern, gain, and overall performance of SAR systems. The present paper sets out to describe the implementation and validation of a phased-array antenna model for Synthetic Aperture Radar Systems (SARAS) in MATLAB R2024a. The antenna model was developed for utilization in the Spanish Earth observation missions PAZ and PRECURSOR-ECO. The antenna model incorporates a number of functions, which are divided into two primary modules: the first of these is the antenna pattern generation (APG) module, and the second is the antenna excitation generation (AEG) module. The present document focuses on the AEG, the function of which is to generate patterns for all required beams. These patterns are optimized and matched to specific calculated masks using an ad hoc genetic algorithm (GA). In consideration of the aforementioned factors, the AEG module generates a set of complex excitations corresponding to the required beam from different satellite operational beams, based on several radiometrically defined parameters.
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ISSN:1424-8220
1424-8220
DOI:10.3390/s25154835