PL EN


Preferencje help
Widoczny [Schowaj] Abstrakt
Liczba wyników
Tytuł artykułu

Robust control of the micro UAV dynamics with an autopilot

Autorzy
Treść / Zawartość
Identyfikatory
Warianty tytułu
Języki publikacji
EN
Abstrakty
EN
This paper presents a nonlinear robust control design procedure for a micro air vehicle, which uses the singular value (μ) and μ-synthesis technique. The optimal robust control law that combines parametric and lumped uncertainties of the micro UAV (unmanned aerial vehicle) which are realized by serial connection of the Kestrel autopilot and the Gumstix microprocessor. Thus, the robust control feedback loops, which handle the uncertainty of aerodynamics derivatives, are used to ensure the robust stability of the UAV local Dynamics in longitudinal and lateral control directions.
Rocznik
Strony
751--761
Opis fizyczny
Bibliogr. 17 poz., rys., tab.
Twórcy
  • Białystok University of Technology, Bialystok, Poland
Bibliografia
  • 1. Aguiar A.P., Hespanha J.P., 2007, Trajectory-tracking and path-following of underactuated autonomous vehicles with parametric modeling uncertainty, IEEE Tran. on Automation Conference, 52, 1362-1379
  • 2. Balas G.J., Packard A.K., and J.T. Harduvel J.T., 1991, Application of μ-synthesis techniques to momentum management and attitude control of the space station, AIAA Guidance, Navigation and Control Conference, New Orleans
  • 3. Burns R.S., 2001, Advanced Control Engineering, Butterworth-Heinemann
  • 4. Gordnier R.E., 2009, High fidelity computational simulation of a membrane wing airfoil, Journal of Fluids and Structures, 25, 897-917
  • 5. Mathworks Inc., www.mathworks.com
  • 6. Micropilot Inc., www.micro-pilot.com
  • 7. Mystkowski A., 2012a, An application of μ-synthesis to control of a small air vehicle – simulation results, Journal of Vibroengineering, 14, 1, 79-86
  • 8. Mystkowski A., 2012b, The robust control of unmanned aerial vehicle, Research project report No, 0029/R/T00/2010/11, conducted in the years: 2010-2013 [in Polish]
  • 9. Mystkowski A., Ostapkowicz P., 2011, Verification of MAV dynamics model with vortex piezo-generators to boundary flow control, Warsaw Inst. of Aviation, 216, 103-125
  • 10. NASA, 1976, Vortex-lattice utilization, NASA SP-405, NASA-Langley, Washington
  • 11. Procerus, Inc., www.procerus.com
  • 12. Tornado 1.0, 2001, User Guide, Reference manual, Relase 2.3
  • 13. Valavanis K.P., 2007, Advances in Unmanned Aerial Vehicles, State of the Art and the Road to Autonomy, Springer, 33
  • 14. www.gumstix.com
  • 15. www.topmodelcz.cz
  • 16. Zhou K., Doyle J., 1998, Essentials of Robust Control, Prentice Hall
  • 17. Zhou K., Doyle J.C., Glover K., 1996, Robust and Optimal Control, Prentice Hall
Typ dokumentu
Bibliografia
Identyfikator YADDA
bwmeta1.element.baztech-36666d13-a490-4fad-ad3b-0eec4e14c0f1
JavaScript jest wyłączony w Twojej przeglądarce internetowej. Włącz go, a następnie odśwież stronę, aby móc w pełni z niej korzystać.