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A control method for nonlinear feedback linearization and its application

  • 2013-09-22
  • 165.15KB
  • Points it Requires : 1

The input/output feedback linearization processing method based on differential geometry is studied and applied to the nonlinear control equation of the aircraft. At the same time, a tracking control scheme is designed for the longitudinal flight trajectory of the aircraft automatic landing. Keywords: nonlinear, feedback linearization, automatic landing

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