Adaptive control augmentation of a missile

Kutluay K. T., Yavrucuk I.

10th IFAC International Workshop on Adaptation and Learning in Control and Signal Processing, ALCOSP 2010, Antalya, Türkiye, 26 - 28 Ağustos 2010, cilt.1, ss.77-82 identifier

  • Yayın Türü: Bildiri / Tam Metin Bildiri
  • Cilt numarası: 1
  • Doi Numarası: 10.3182/20100826-3-tr-4015.00017
  • Basıldığı Şehir: Antalya
  • Basıldığı Ülke: Türkiye
  • Sayfa Sayıları: ss.77-82
  • Anahtar Kelimeler: Adaptive augmentation, Adaptive control, Dynamic inversion, Output redefinition
  • Orta Doğu Teknik Üniversitesi Adresli: Evet

Özet

Adaptive control augmentation can be used for the controller design of air vehicles, eliminating the need for a detailed design process and accurate model data. This paper presents the application of the L1 adaptive control augmentation system to a baseline autopilot of a missile, which is designed with dynamic model inversion at a single flight condition. The output redefinition approach is used in the inversion process of the non-minimum phase transfer functions. The resulting controllers are examined through high fidelity, nonlinear, 6 D.o.F. simulations. © 2010 IFAC.