This chapter introduces geolocation of emitter of earth by a single satellite by kinematic parameters which include frequency, frequency changing rate, time of arrival(TOA), interferometer phase rate of changing information. The geolocation error is simulated and the Cramer‐Rao lower bound(CRLB) of geolocation error is also analyzed.


    Access

    Check access

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Single‐Satellite Geolocation System Based on the Kinematic Principle


    Contributors:
    Guo, Fucheng (author) / Fan, Yun (author) / Zhou, Yiyu (author) / Zhou, Caigen (author) / Li, Qiang (author)

    Published in:

    Publication date :

    2014-04-08


    Size :

    25 pages




    Type of media :

    Article/Chapter (Book)


    Type of material :

    Electronic Resource


    Language :

    English




    Single‐Satellite Geolocation System Based on Direction Finding

    Guo, Fucheng / Fan, Yun / Zhou, Yiyu et al. | Wiley | 2014


    Fundamentals of Satellite Orbit and Geolocation

    Guo, Fucheng / Fan, Yun / Zhou, Yiyu et al. | Wiley | 2014


    Automatic Geolocation Correction of Satellite Imagery

    Ozcanli, O. C. / Dong, Y. / Mundy, J. L. et al. | British Library Online Contents | 2016


    Sensitivity analysis of dual-satellite geolocation

    Pattison, T. / Chou, S.I. | IEEE | 2000


    Dual‐Satellite Geolocation Based on TDOA and FDOA

    Guo, Fucheng / Fan, Yun / Zhou, Yiyu et al. | Wiley | 2014