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      Sensitivity Analysis of Extended and Unscented Kalman Filters for Attitude Estimation

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          Unscented Filtering for Spacecraft Attitude Estimation

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            Applying the unscented Kalman filter for nonlinear state estimation

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              An integrated GPS/MEMS-IMU navigation system for an autonomous helicopter

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                Author and article information

                Journal
                Journal of Aerospace Information Systems
                Journal of Aerospace Information Systems
                American Institute of Aeronautics and Astronautics (AIAA)
                2327-3097
                March 2013
                March 2013
                : 10
                : 3
                : 131-143
                Article
                10.2514/1.54899
                5a19b642-1c49-4f9a-9a8e-dbbc90bdeb99
                © 2013
                History

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