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Nonlinear Tracking Controller Design for Unmanned Helicopters

  • Ioannis A. RaptisEmail author
  • Kimon P. Valavanis
Part of the Intelligent Systems, Control and Automation: Science and Engineering book series (ISCA, volume 45)

Abstract

The previous Chapter presented a tracking controller of the position and heading of a helicopter based on the linearized helicopter dynamics. The adopted parametric linear model, on which the flight controller is based on, represented the quasi steady state behavior of the helicopter dynamics at hover.

Keywords

Error Dynamic Attitude Dynamic Main Rotor Thrust Vector Tail Rotor 
These keywords were added by machine and not by the authors. This process is experimental and the keywords may be updated as the learning algorithm improves.

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Copyright information

© Springer Science+Business Media B.V. 2011

Authors and Affiliations

  1. 1.Department of Electrical and Computer EngineeringGeorgia Institute of TechnologyAtlantaUSA
  2. 2.Department of Electrical and Computer Engineering, and, Department of Computer Science, School of Engineering and Computer ScienceUniversity of DenverDenverUSA

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