Nasze serwisy używają informacji zapisanych w plikach cookies. Korzystając z serwisu wyrażasz zgodę na używanie plików cookies zgodnie z aktualnymi ustawieniami przeglądarki, które możesz zmienić w dowolnej chwili. Więcej informacji odnośnie plików cookies.

Obowiązek informacyjny wynikający z Ustawy z dnia 16 listopada 2012 r. o zmianie ustawy – Prawo telekomunikacyjne oraz niektórych innych ustaw.

Wyłącz komunikat

 
 

Logowanie

Logowanie za pomocą Centralnej Usługi Uwierzytelniania PRz. Po zakończeniu pracy nie zapomnij zamknąć przeglądarki.

Mechanika

Mechanika
85 (4/13), DOI: 10.7862/rm.2013.49

Reaction shaping of the unmanned aerial vehicle on the operator remote steering signals

Andrzej Tomczyk

DOI: 10.7862/rm.2013.49

Abstract

Remote manual control of unmanned aerial vehicle is used more often during take-of and landing phases. Depends on UAV take-off mass and speed (total energy) the potential crash can be very dangerous for an airplane and environment. So, handling qualities of UAV is important from the user point of view. In many cases the dynamic properties of remote controlling UAV are not suitable for obtaining the desired properties of the handling qualities from operator's point of view. In this case, the control augmentation system (CAS) should be applied. The method of UAV handling qualities shaping is presented in this paper. The main idea of this method is that UAV reaction on the operator steering signals should be similar - almost the same – as the reaction of the „ideal” remote control aircraft. The model of following method was used for controller parameters calculations. The numerical example concerns the medium size UAV MP-02A Czajka applied as an aerial observer system.

Full text (pdf)

References

  1. Austin R.: Unmanned aircraft systems: UAVS Design. Development and Deployment, AIAA Education Series, 2010.
  2. Bernhard R.K., Shappee E., Marshall D.M.: Introduction to unmanned aircraft systems. CRC Press, 2011.
  3. Hamilton J.: UAVs: Unmanned aerial vehicles. ABDO, 2012.
  4. Newcome L.R.: Unmanned aviation. Library of Flight, 2004.
  5. Stevens B.L., Lewis F.L.: Aircraft control and simulation. J. Wiley & Sons, 2004.
  6. Gruszecki J. (ed.): Unmanned aerial vehicles. Control and navigation systems. Oficyna Wydawnicza Politechniki Rzeszowskiej, Rzeszów 2002 (in Polish).
  7. Tomczyk A., Gruszecki J.: Preliminary project of the autonomous landing system for unmanned aircraft. AIAA-SAE Paper 99-01-5524, World Aviation Congress & Exposition, San Francisco 1999.
  8. Tomczyk A.: In-flight tests of navigation and control system of unmanned aerial vehicle. Aircraft Eng. Aerospace Technol.: An Inter. J., 75 (2003), 581-587.
  9. Tomczyk A.: Experimental fly-by-wire control system for general aviation aircraft. AIAA Paper No. 2003-5776, 2003.
  10. Tomczyk A.: Facilitated airplane – project and preliminary in-flight experiments. Aerospace Sci. Technol., 8 (2004), 469-477.
  11. Tomczyk A., Rzucidło P.: Indirect flight control systems for general aviation aircraft. Oficyna Wydawnicza Politechniki Rzeszowskiej, Rzeszów 2011 (in Polish).
  12. Astrom K.J., Wittenmark B.: Adaptive control. Addison-Wesley Publishing Company, 1989.
  13. Huang C., Tylock J.: Comparison of modern model-following aircraft control techniques. AIAA-93-3843, AIAA Guidance, Navigation and Control Conference, Monterey 1993, pp. 1274-1284.
  14. Kreindler E., Rothschild D.: Model-following in linear-quadratic optimization. AIAA Journal, 14 (1976), 835-842.
  15. Tomczyk A.: Digital flight control systems. Oficyna Wydawnicza Politechniki Rzeszowskiej, Rzeszów 1999 (in Polish).
  16. Gill P.E., Murray W., Wright H.M:. Practical optimization. Academic Press, 1981.
  17. Lambregts A.A.: Fundamentals of FBW augmented manual control. SAE Paper, SAE-2005-01-3419, 2005.
  18. Pieniążek J.: Active command interfaces in fly-by-wire control. Systems Science, 34 (2008), 68-75.

About this Article

TITLE:
Reaction shaping of the unmanned aerial vehicle on the operator remote steering signals

AUTHORS:
Andrzej Tomczyk

AUTHORS AFFILIATIONS:
Rzeszow University of Technology

JOURNAL:
Mechanika
85 (4/13)

KEY WORDS AND PHRASES:
unmanned aerial vehicle, controlling, augmentation system, autopilot

FULL TEXT:
http://doi.prz.edu.pl/pl/pdf/mechanika/61

DOI:
10.7862/rm.2013.49

URL:
http://dx.doi.org/10.7862/rm.2013.49

RECEIVED:
2013-09-15

COPYRIGHT:
Publishing House of Rzeszow University of Technology Powstańców Warszawy 12, 35-959 Rzeszow

POLITECHNIKA RZESZOWSKA im. Ignacego Łukasiewicza; al. Powstańców Warszawy 12, 35-959 Rzeszów
tel.: +48 17 865 11 00, fax.: +48 17 854 12 60
Administrator serwisu:

Deklaracja dostępności | Polityka prywatności