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    Robust Estimation of UAV Dynamics in the Presence of Measurement Faults 

    Source: Journal of Aerospace Engineering:;2012:;Volume ( 025 ):;issue: 001
    Author(s): Chingiz Hajiyev; Halil Ersin Soken
    Publisher: American Society of Civil Engineers
    Abstract: This study introduces a robust Kalman filter (RKF) with a filter-gain correction for cases of measurement malfunctions. Using defined variables called measurement-noise scale factors, the faulty measurements are taken into ...
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    Adaptive Tuning of the Unscented Kalman Filter for Satellite Attitude Estimation 

    Source: Journal of Aerospace Engineering:;2015:;Volume ( 028 ):;issue: 003
    Author(s): Halil Ersin Soken; Shin-ichiro Sakai
    Publisher: American Society of Civil Engineers
    Abstract: Determining the process noise covariance of the unscented Kalman filter (UKF) is a difficult procedure. The analytical approximation method gives satisfactory results in certain cases, but it fails when generalized for the ...
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    Nontraditional Attitude Filtering with Simultaneous Process and Measurement Covariance Adaptation 

    Source: Journal of Aerospace Engineering:;2019:;Volume ( 032 ):;issue: 005
    Author(s): Chingiz Hajiyev; Halil Ersin Soken; Demet Cilden-Guler
    Publisher: American Society of Civil Engineers
    Abstract: This study discusses simultaneous adaptation of the process and measurement noise covariance matrixes for a nontraditional attitude filtering algorithm. The nontraditional attitude filtering algorithm integrates the singular ...
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    DSpace software copyright © 2002-2015  DuraSpace
    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
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    DSpace software copyright © 2002-2015  DuraSpace
    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
    yabeshDSpacePersian