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.


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    Title :

    Configuration, Orbit Design of InSAR Formation Based on Mean Elements


    Contributors:
    Jinxiu Zhang, (author) / Xibin Cao, (author) / Jihe Wang, (author) / Xiaohui Lin, (author)


    Publication date :

    2009-04-01


    Size :

    983685 byte




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English




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