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NASA NTRS · 20140011532

Output Feedback M-MRAC Backstepping With Aerospace Applications

Abstract

The paper presents a certainty equivalence output feedback backstepping adaptive control design method for the systems of any relative degree with unmatched uncertainties without over-parametrization. It uses a fast prediction model to estimate the unknown parameters, which is independent of the control design. It is shown that the system's input and output tracking errors can be systematically decreased by the proper choice of the design parameters. The approach is applied to aerospace control problems and tested in numerical simulations.

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BibTeXRIS

Stepanyan, Vahram, Krishnakumar, Kalmanje Sriniva. 2014-01-13. Output Feedback M-MRAC Backstepping With Aerospace Applications. https://ntrs.nasa.gov/citations/20140011532

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