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    Attitude estimation based on fusion of gyroscopes and single antenna GPS for small UAVs under the influence of vibration

    An attitude estimation method is presented for small unmanned aerial vehicles (UAVs) powered by a piston engine which is the major source of vibration. Vibration of the engine significantly degrades the accura...

    Ying-Chih Lai, Shau-Shiun Jan in GPS Solutions (2011)