Mechanical Vibrations on a Deployable Nanosatellite Antenna: SAR Performance Analysis
2024 18th European Conference on Antennas and Propagation (EuCAP)(2024)
Abstract
The mechanical vibrations of a high-strain glass-fibre composite deployable X-band synthetic aperture radar (SAR) antenna structure are investigated using a finite element method. The antenna is approximately
$\mathrm{2}\ \mathrm{m}\times \mathrm{0}.\mathrm{3}\ \mathrm{m}$
, and exhibits natural frequencies at 2.8 Hz and 7.6 Hz. The radiation patterns for a reflectarray formed from the structure are calculated using a ray-tracing approach for the nominal and mechanically deformed cases. The mechanically deformed antenna pattern is defocused, and a SAR system model shows this reduces the signal-to-noise ratio of a point scattering target by approximately 6 dB.
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Key words
deployable antenna,synthetic aperture radar,reflectarray,mechanical vibrations,small satellites
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