Adaptive control design methodology for nonlinear-in-control systems in aircraft applications

Amanda Young, Chengyu Cao, Vijay Patel, Naira Hovakimyan, Eugene Lavretsky

Research output: Contribution to journalArticle

Abstract

An adaptive control design method for both short-period and lateral/directional control of a fighter aircraft is presented. The proposed method is directly applicable to flight control of vehicles with state-dependent and nonlinear-in-control uncertain dynamics. The developed design approach uses a specialized set of radial basis function approximators and Lyapunov-based adaptive laws to compensate for the unknown control-dependent nonlinearities. The adaptive controller is defined as a solution of fast dynamics, which verifies the assumptions of Tikhonov's theorem from singular perturbations theory. Simulations illustrate the theoretical findings.

Original languageEnglish (US)
Pages (from-to)1770-1782
Number of pages13
JournalJournal of Guidance, Control, and Dynamics
Volume30
Issue number6
DOIs
StatePublished - 2007
Externally publishedYes

ASJC Scopus subject areas

  • Control and Systems Engineering
  • Aerospace Engineering
  • Space and Planetary Science
  • Electrical and Electronic Engineering
  • Applied Mathematics

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