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The application of nonlinear inverse dynamics for aircraft control at high angles of attack

Złocka M.

Research Bulletin / Warsaw University of Technology, Institute of Aeronautics and Applied Mechanics

1999

nr 9

179-184

The main objective of this work is the elimination of the wing-rock phenomenon during the aircraft motion at high angles of attack. Two wing-rock models having three or one degree of freedom are considered. In the paper, the nonlinear control laws have been synthesised for stabilization of the steady horizontal motion of the aircraft. The synthesis is based on the nonlinear inverse dynamics. As an example the numerical simulation of the controlled motion is carried out employing the aerodynamic and mass data of the F-16 aircraft.