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Reconfiguration of Unmanned Aircraft Control System Cover

Reconfiguration of Unmanned Aircraft Control System

By: Marcin Żugaj  
Open Access
|May 2019

References

  1. [1] Goetzendorf-Grabowski, T., Frydrychewicz, A., Goraj, Z., et al., 2006, “MALE UAV design of an increased reliability level,” Aircraft Engineering and Aerospace Technology: An International Journal, vol. 78, No 3, pp. 226-235.10.1108/17488840610663693
  2. [2] Lin, X., Fulton, N., and Horn, M., 2014, „Quantification of high level safety criteria for civil unmanned aircraft systems;” Proceedings of IEEE Aerospace Conference, Big Sky, March 1-8, pp. 1-13.10.1109/AERO.2014.6836463
  3. [3] Loh, R., Bian, Y., and Roe, T., 2009, „UAVs in civil airspace: Safety requirements;” IEEE Aerospace and Electronic Systems Magazine, 24, January, pp. 5-17.10.1109/MAES.2009.4772749
  4. [4] Goraj, Z., 2014, “A specialized UAV for surveillance in windy, turbulent environment of the Antarctic coast,” Proceedings of the 29th Congress of the International Council of the Aeronautical Sciences Vol I-VI, Curran Associates, Inc, pp. 1-13.
  5. [5] Steinberg, M., 2005, „A historical overview of research in reconfigurable flight control;” Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 219, April, pp. 263-275.10.1243/095441005X30379
  6. [6] Kozak, V., Shevchuk, D., Vovk, V., and Levchenko, M., 2014, „Automation of aircraft control Rreconfiguration in flight special situations;” Proceedings of IEEE 3rd International Conference on Methods and Systems of Navigation and Motion Control, Kiev, October 14-17, pp. 14-17, October 2014.10.1109/MSNMC.2014.6979759
  7. [7] Yang, Z., Hua, S., Hongzhuan, Q., and Chengrui, L., 2010, „Control reconfigurability of nonlinear system based on control redundancy;” 10th IEEE International Conference on Industrial Informatics (INDIN), Beijing, July 25-27, pp. 815-820.10.1109/INDIN.2012.6301366
  8. [8] Burcham, B., 1997, „Landing safely when flight controls fail;” Aerospace America, pp. 20-23.
  9. [9] Naskar, A., Patra, S., and Sen, S., 2015, „Reconfigurable Direct Allocation for Multiple Actuator Failures;” IEEE Transactions on Control Systems Technology, 1(23), January, pp. 397-405.10.1109/TCST.2014.2321665
  10. [10] Xiao-hui, Q., and Hong-tao, Z., 2011, „The Design od Adaptive Sliding Mode Control Law on Reconfigurable Flight Control System;” International Conference on Electronics, Communications and Control (ICECC), Ningbo, September 9-11, pp. 532-536.10.1109/ICECC.2011.6067617
  11. [11] Fekri, S., Gu, D., and Postlethwaite, I., 2009, „Lateral Imbalance Detection on a UAV Based on Multiple Models;” Joint 48th IEEE Conference on Decision and Control and 28th Chinese Control Conference, Shanghai, December 16-18, pp. 8488-8493.10.1109/CDC.2009.5399576
  12. [12] Nizioł, J., 2005, Dynamika układów mechanicznych (Dynamics of mechanical systems), Komitet Mechaniki PAN (Mechanics Committee of the Polish Academy of Sciences). Instytut Podstawowych Problemów Techniki Polskiej Akademii Nauk (Institute of Fundamental Technological Problems of the Polish Academy of Sciences), Warsaw.
  13. [13] Goraj, Z., 2014, “Flight dynamics models used in different national and internationals projects,” Aircraft Engineering and Aerospace Technology, Volume: 86 Issue: 3.10.1108/AEAT-02-2013-0036
  14. [14] Zugaj, M., and Narkiewicz, J., 2009, „Autopilot for reconfigurable flight control system;” ASCE Journal of Aerospace Engineering, 22, January, pp. 78-84.10.1061/(ASCE)0893-1321(2009)22:1(78)
  15. [15] Żugaj, M., Godłoża, D., 2016, „Analiza właściwości dynamicznych samolotu bezzałogowego w stanie awarii systemu sterowania;” (Analysis of dynamic properties of an unmanned aircraft in a failure state). Mechanika w Lotnictwie (Mechanics in Aeronautics) ML-XVII, vol. 2, Warszawa, pp. 275-286.
  16. [16] Jategaonkar, R., V., 2006, Flight Vehicle System Identification, A Time Domain Methodology, American Institute of Aeronautics and Astronautics, Reston, Virginia.10.2514/4.866852
  17. [17] Yechout, T., R., 2003, Introduction to Aircraft Flight Mechanics: Performance, Static Stability, Dynamic Stability, and Classical Feedback Control, American Institute of Aeronautics and Astronautics, Reston, Virginia.
Language: English
Page range: 80 - 96
Published on: May 31, 2019
In partnership with: Paradigm Publishing Services
Publication frequency: 4 issues per year

© 2019 Marcin Żugaj, published by ŁUKASIEWICZ RESEARCH NETWORK – INSTITUTE OF AVIATION
This work is licensed under the Creative Commons Attribution-NonCommercial-NoDerivatives 3.0 License.