Comparison of Classical and Modern Landing Control System for a Small Unmanned Aerial Vehicle

Nugroho L.

International Conference on Computer, Control, Informatics and Its Applications (IC3INA), Bandung, Endonezya, 21 - 23 Ekim 2014, ss.187-192 identifier

  • Yayın Türü: Bildiri / Tam Metin Bildiri
  • Basıldığı Şehir: Bandung
  • Basıldığı Ülke: Endonezya
  • Sayfa Sayıları: ss.187-192
  • Orta Doğu Teknik Üniversitesi Adresli: Evet

Özet

Research presented in the following paper contrasted the modern optimal robust control method with classical one, applied for a landing control system of a small unmanned aerial vehicle. Philosophically speaking, the optimal control used H-2 method meets excellent dynamic performance, while the robustness given by the H infinity method diminish the effect of disturbance to the performance output. Accordingly, implemented mixed H2/H infinity optimal robust control method in this paper appear to meet a balancing result between performance and robustness stability.