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  • End-to-end space system demonstration concepts for a distributed SAR by small formation flying satellites

    Paper number

    IAC-19,B4,7,8,x50724

    Author

    Dr. Alfredo Renga, Italy, University of Naples "Federico II"

    Coauthor

    Dr. Giancarmine Fasano, Italy, University of Naples "Federico II"

    Coauthor

    Mr. Marco Grasso, Italy, University of Naples "Federico II"

    Coauthor

    Dr. Maria Daniela Graziano, Italy, University of Naples "Federico II"

    Coauthor

    Prof. Michele Grassi, Italy, University of Naples "Federico II"

    Coauthor

    Prof. Antonio Moccia, Italy, University of Naples "Federico II"

    Coauthor

    Dr. Giancarlo Rufino, Italy, University of Naples "Federico II"

    Coauthor

    Dr. Roberto Opromolla, Italy, University of Naples "Federico II"

    Year

    2019

    Abstract
    The paper discusses a mission concept for end-to-end space demonstration of Distributed Synthetic Aperture Radar (DSAR) principles and operations. This is realized by 3 satellites working in X-band, flying in a LEO close formation. One satellite embarks a Tx/Rx radar, i.e. it is a monostatic SAR. The other two satellites are Rx-only items. The system is expected to feature formation flying capabilities: it must be able to guarantee formation control and to perform formation reconfiguration maneuvers. Both Tx/Rx and Rx-only satellites are expected to be in the range of micro-satellite class (<100 kg). From the DSAR perspective, starting from the design of a general purpose monostatic SAR targeted to achieve 8m x 8m resolution on the ground, from an orbit altitude of 550 km, DSAR properties are exploited to demonstrate performance improvement, namely the achievement of 4m x 4m resolution with the same Noise Equivalent Sigma Zero (NESZ) requirement, testing suitable combinations of DSAR techniques like Signal-to-Noise Ratio (SNR) enhancement, Pulse Repetition Frequency (PRF) reduction, Coherence Resolution Enhancement (CRE). Moreover, at the nominal 8m x 8m resolution, 3D imaging and Ground Moving Target Indication (GMTI) techniques can be also tested. Specific solution for time and phase synchronization enabling bistatic operations are detailed in the paper, together with the individuation of techniques and sensors for accurate absolute and relative positioning and pointing.
    Abstract document

    IAC-19,B4,7,8,x50724.brief.pdf

    Manuscript document

    IAC-19,B4,7,8,x50724.pdf (🔒 authorized access only).

    To get the manuscript, please contact IAF Secretariat.