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, Turkey, 26 - 28 August 2010, vol.1, pp.77-82, (Full Text) identifier

  • Publication Type: Conference Paper / Full Text
  • Volume: 1
  • Doi Number: 10.3182/20100826-3-tr-4015.00017
  • City: Antalya
  • Country: Turkey
  • Page Numbers: pp.77-82
  • Keywords: Adaptive augmentation, Adaptive control, Dynamic inversion, Output redefinition
  • Middle East Technical University Affiliated: Yes

Abstract

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.