Configuration, Orbit Design of InSAR Formation Based on Mean Elements

A mission requirements-based configuration method of interferometric synthetic-aperture radar (InSAR) formation to design dual-satellite formation by mean orbital elements is derived. The configuration and initial orbital elements of two coordinated running satellites InSAR formation are designed wh...

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Published in:IEEE transactions on aerospace and electronic systems 2009-04, Vol.45 (2), p.747-752
Main Authors: Zhang, Jinxiu, Cao, Xibin, Wang, Jihe, Lin, Xiaohui
Format: Article
Language:English
Subjects:
Air traffic control
Aircraft components
Costs
Design engineering
Design methodology
Digital elevation models
Electronic systems
Orbital calculations
Orbital elements
Orbits
Passive radar
Radar
Running
Satellites
Space technology
Spaceborne radar
Synthetic aperture radar
Synthetic aperture radar interferometry
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cited_by cdi_FETCH-LOGICAL-c356t-d7acee511f1f4079ae4d2c4e0e5f7016d026449008991f93633976520192cbf13
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container_title IEEE transactions on aerospace and electronic systems
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creator Zhang, Jinxiu
Cao, Xibin
Wang, Jihe
Lin, Xiaohui
description A mission requirements-based configuration method of interferometric synthetic-aperture radar (InSAR) formation to design dual-satellite formation by mean orbital elements is derived. The configuration and initial orbital elements of two coordinated running satellites InSAR formation are designed when system parameters, such as the resolution of slant distance, latitude domain of ground coverage area, and the side-looking angle of the synthetic-aperture radar (SAR) beam center, are given.
doi_str_mv 10.1109/TAES.2009.5089555
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source IEEE Electronic Library (IEL) Journals
subjects Air traffic control
Aircraft components
Costs
Design engineering
Design methodology
Digital elevation models
Electronic systems
Orbital calculations
Orbital elements
Orbits
Passive radar
Radar
Running
Satellites
Space technology
Spaceborne radar
Synthetic aperture radar
Synthetic aperture radar interferometry
title Configuration, Orbit Design of InSAR Formation Based on Mean Elements
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