Synthesis of a Controller Built on the Principle of Inverse Dynamics and Identification of a Nonlinear Model of Longitudinal Motion in Offline Mode

Abstract

This report is dedicated to the design of a controller based on the principle of inverse dynamics and the offline identification of the coefficients of a supersonic transport (SST) aircraft’s linear longitudinal dynamics model based on the results of measuring the nonlinear mathematical model’s responses. A landing task under the influence of atmospheric disturbances is considered.