Robust Model Following Control Design for Missile Roll Autopilot

Gezer R. B., KUTAY A. T.

United-Kingdom-Automatic-Control-Council (UKACC) 10th International Conference on Control (CONTROL), Loughborough, Birleşik Krallık, 9 - 11 Temmuz 2014, ss.7-12 identifier identifier

  • Yayın Türü: Bildiri / Tam Metin Bildiri
  • Basıldığı Şehir: Loughborough
  • Basıldığı Ülke: Birleşik Krallık
  • Sayfa Sayıları: ss.7-12
  • Orta Doğu Teknik Üniversitesi Adresli: Evet

Özet

This paper presents a robust model following control method augmented with error integration and Luenberger observer for anti-air missile roll autopilot designed using optimal control laws. The design is shown to be robust to external disturbance, noisy measurements and sensor lags by frequency domain analysis. The regulation performance of the controller is presented by simulations.