2015 European Radar Conference (EuRAD) 2015
DOI: 10.1109/eurad.2015.7346324
|View full text |Cite
|
Sign up to set email alerts
|

Design considerations on a sparse array antenna for Ka-band spaceborne SAR applications

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
3
1

Citation Types

0
4
0

Year Published

2016
2016
2024
2024

Publication Types

Select...
1
1
1

Relationship

1
2

Authors

Journals

citations
Cited by 3 publications
(4 citation statements)
references
References 6 publications
0
4
0
Order By: Relevance
“…It is shown that a density taper along the elevation dimension with a fill factor of 90% with respect to the benchmark array still allows satisfying the mask for the receive pattern. Such a taper in combination with the approach described in [2] to implement sparsity along the azimuth dimension of the antenna would allow for a substantial reduction of the active modules. Topics of further investigation are the fine-tuning of the density tapers to avoid mask violations while scanning, the verification of the 2D patterns for scanning off elevation plane, and the combination of sparsity in elevation and azimuth.…”
Section: Discussionmentioning
confidence: 99%
See 3 more Smart Citations
“…It is shown that a density taper along the elevation dimension with a fill factor of 90% with respect to the benchmark array still allows satisfying the mask for the receive pattern. Such a taper in combination with the approach described in [2] to implement sparsity along the azimuth dimension of the antenna would allow for a substantial reduction of the active modules. Topics of further investigation are the fine-tuning of the density tapers to avoid mask violations while scanning, the verification of the 2D patterns for scanning off elevation plane, and the combination of sparsity in elevation and azimuth.…”
Section: Discussionmentioning
confidence: 99%
“…In [2] the problem of introducing sparsity in a Ka-band phased-array SAR antenna able to scan +/-10° in elevation and +/-2° in azimuth was presented. The general mission and antenna requirements are reported in [2].…”
Section: Introduction and Problem Definitionmentioning
confidence: 99%
See 2 more Smart Citations