Nonlinear control of VTOL UAVs incorporating flapping dynamics

By Sammy Omari, Minh-Duc Hua, G. Ducard, Tarek Hamel. 2013

72 citations recorded by the source corpus.

This paper presents the design and evaluation of a nonlinear control scheme for multirotor helicopters that takes first-order drag effects into account explicitly. A dynamic model including the blade flapping and induced drag forces is presented. Based on this model, a hierarchical nonlinear controller is designed to actively compensates for the nonlinear effects these drag forces. Reported simulation and experimental results indicate the significant performance improvement of the proposed drag-augmented control scheme with respect to a conventional nonlinear controller. For completeness, an offline procedure allowing for efficiently identifying the drag parameters is proposed.

Subfields: Aerospace Engineering, Control and Systems Engineering, Ocean Engineering

How researchers see this paper

The researchers whose trusted networks rank it highest, strongest advocate first. Every researcher gets a different order.

In Aerospace Engineering

  1. Davide Scaramuzza
  2. Markus Achtelik
  3. Roland Yves Siegwart
  4. Matthias Faessler
  5. Moses Bangura
  6. Michael Burri
  7. Guoquan Huang
  8. Robert E. Mahony

In Control and Systems Engineering

  1. Davide Scaramuzza
  2. Moses Bangura
  3. Markus Achtelik
  4. Roland Yves Siegwart
  5. Matthias Faessler
  6. Robert E. Mahony
  7. Antonio Franchi
  8. Michael Burri

In Ocean Engineering

  1. Davide Scaramuzza
  2. Roland Yves Siegwart
  3. Markus Achtelik
  4. Robert E. Mahony
  5. Moses Bangura
  6. Sergey I. Nikolenko
  7. S. Microtechnique
  8. Mohammad Rostami

Citations in the corpus