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    Single Station Antenna–Based Spacecraft Orbit Determination via Robust EKF against the Effect of Measurement Matrix Singularity 

    Source: Journal of Aerospace Engineering:;2015:;Volume ( 028 ):;issue: 001
    Author(s): Ahmet Sofyalı; Chingiz Hajiyev
    Publisher: American Society of Civil Engineers
    Abstract: In this study, a robust extended Kalman filter (EKF) for estimation of a spacecraft’s position and velocity by single station antenna tracking data against the effect of measurement matrix singularity is proposed. The ...
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    Active Fault-Tolerant Control of UAV Dynamics against Sensor-Actuator Failures 

    Source: Journal of Aerospace Engineering:;2016:;Volume ( 029 ):;issue: 004
    Author(s): Fikret Caliskan; Chingiz Hajiyev
    Publisher: American Society of Civil Engineers
    Abstract: In this paper, an active fault-tolerant flight control system against sensor/actuator failures for unmanned aerial vehicles (UAVs) is proposed. First, an approach to detecting and isolating UAV sensor failures affecting ...
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    Active Fault-Tolerant Control of UAV Dynamics against Sensor-Actuator Failures 

    Source: Journal of Aerospace Engineering:;2016:;Volume ( 029 ):;issue: 004
    Author(s): Fikret Caliskan; Chingiz Hajiyev
    Publisher: American Society of Civil Engineers
    Abstract: In this paper, an active fault-tolerant flight control system against sensor/actuator failures for unmanned aerial vehicles (UAVs) is proposed. First, an approach to detecting and isolating UAV sensor failures affecting ...
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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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    SVD-Aided UKF Adaptation for Nanosatellite Attitude Estimation under Uncertain Process Noise Conditions 

    Source: Journal of Aerospace Engineering:;2025:;Volume ( 038 ):;issue: 002:;page 04024121-1
    Author(s): Chingiz Hajiyev; Demet Cilden-Guler
    Publisher: American Society of Civil Engineers
    Abstract: In this work, the adaptation of the process noise covariance matrix for the nontraditional attitude filtering technique is discussed. The nontraditional attitude filtering technique integrates the unscented Kalman filter ...
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    Aircraft Icing Detection, Identification, and Reconfigurable Control Based on Kalman Filtering and Neural Networks 

    Source: Journal of Aerospace Engineering:;2008:;Volume ( 021 ):;issue: 002
    Author(s): Fikret Caliskan; Rahmi Aykan; Chingiz Hajiyev
    Publisher: American Society of Civil Engineers
    Abstract: Flight in all weather conditions has necessitated correctly detecting icing and taking reasonable measures against it. This work aims at the detection and identification of airframe icing based on statistical properties ...
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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
    yabeshDSpacePersian
     

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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