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A numerical method for the solution of the error-feedback output regulation problem

A numerical method to solve the so-called regulator equation is presented here. The regulator equation arises when solving the output regulation problem. This equation consists of partial differential equations combined with algebra...

BC - Teorie a systémy řízení

  • 2006
  • D
Result

Real-Time Error-Feedback Output Regulation of Nonhyperbolically Nonminimum Phase System

A real time implementation of an error feedback output regulation problem for the gyroscopical platform is presented here. It is based on a numerical method for the solution of partialdifferential equations combined with al...

BC - Teorie a systémy řízení

  • 2007
  • O
Result

Real-Time Error-Feedback Output Regulation of Nonhyperbolically Nonminimum Phase System

A real time implementation of an error feedback output regulation problem for the gyroscopical platform is presented here. It is based on a numerical method for the solution of partialdifferential equations combined with al...

BC - Teorie a systémy řízení

  • 2007
  • D
Result

Finite difference solution of discrete-time regulator equation and its application to digital output regulation problem

A method for the solution of the regulator equation for the discrete-time nonlinear output regulation problem is presented. This method is based on solution zero tracking error is replaced by an error func...

BC - Teorie a systémy řízení

  • 2009
  • D
Result

@EROiDENT 1.2

Application for the identification of flight parameters using the maximum likelihood method.

JU - Aeronautika, aerodynamika, letadla

  • 2010
  • R
Result

Intrusion Detection Using Error Correcting Output Code Based Ensemble

and AdaBoost ensemble methods. We proposed a new hybrid ensemble for intrusion detection based on Error Correcting Output Code (ECOC) approach. (C) 2014 IEEEIntrusion Detection System is an essential part in computer secur...

IN - Informatika

  • 2014
  • D
  • Link
Result

Aerodynamic characteristics identification of atmospheric airplane from flight measurement results

The thesis deals with aerodynamic characteristics identification from flight measurement. The topic is part of flight mechanic – handling qualities. The first theoretic part consists of three identification methods description: Error

JU - Aeronautika, aerodynamika, letadla

  • 2013
  • O
Result

Manually Flagged Errors in WMT09 Test Set

A collection of outputs of 4 machine translation systems. Errors in the output are manually flagged and classified.

AI - Jazykověda

  • 2009
  • R
Result

Approximation of Binary-Valued Functions by Networks of Finite VC Dimension

Distributions of errors in approximation of binary-valued functions by networks with sets of input-output functions of finite VC dimension is investigated. Conditions on concentration of approximation errors around their me...

Computer sciences, information science, bioinformathics (hardware development to be 2.2, social aspect to be 5.8)

  • 2023
  • D
  • Link
Result

Automatic Translation Error Analysis

We propose a method of automatic identification of various error types in machine translation output. The approach is mostly based on monolingual word alignment of the hypothesis and the reference translation. In addition t...

AI - Jazykověda

  • 2011
  • Jx
  • Link
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