21–40 of 79 hits
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    Integrated NRM/EKF for LEO satellite GPS based orbit determination

    Bagci, Murat / Hajiyev, Chingiz | IEEE | 2016

    Active Fault-Tolerant Control of UAV Dynamics against Sensor-Actuator Failures

    Caliskan, Fikret / Hajiyev, Chingiz | ASCE | 2016

      Active Fault-Tolerant Control of UAV Dynamics against Sensor-Actuator Failures

      Caliskan, Fikret | Online Contents | 2016
      Contributors: Hajiyev, Chingiz

    Swarm Architecture of UAVs

    Erkec, Tuncay Yunus / Hajiyev, Chingiz | Springer Verlag | 2022

    Sensor and control surface/actuator failure detection and isolation applied to F-16 flight dynamic

    Hajiyev, Chingiz / Caliskan, Fikret | Emerald Group Publishing | 2005

    SVD-Aided EKF for Nanosatellite Attitude Estimation Based on Kinematic Relations

    Cilden-Guler, Demet / Hajiyev, Chingiz | Springer Verlag | 2023

    Satellite Formation Flight Via NRM and EKF State Estimation Method

    Erkec, Tuncay Yunus / Hajiyev, Chingiz | Springer Verlag | 2023

    Fault-Tolerant Estimation of Relative Motion of Satellites in Cluster

    Erkec, Tuncay Yunus / Hajiyev, Chingiz | Springer Verlag | 2023

    Fault-tolerant state estimation methods of cluster satellites

    Yunus Erkec, T. / Hajiyev, Chingiz | Elsevier | 2022

    Innovation approach to detect the faults in multidimensional dynamic systems

    Hajiyev, Chingiz / Okatan, Ali | Tema Archive | 2010

    RKF-based fault tolerant integrated INS/radar altimeter

    Hajiyev, Chingiz / Saltoglu, Remzi | Emerald Group Publishing | 2004

      RKF-based fault tolerant integrated INS-radar altimeter

      Hajiyev, Chingiz | Online Contents | 2004

    Nanosatellite attitude estimation using Kalman-type filters with non-Gaussian noise

    Cilden-Guler, Demet / Raitoharju, Matti / Piche, Robert et al. | Elsevier | 2019