Active suppression of freeplay aeroelastic vibrations of ailerons by robust control methods with incomplete measurements

Abstract

Purpose

The purpose of this paper is to analyze the active suppression of the nonlinear aeroelastic vibrations of ailerons caused by freeplay by robust H_∞ and linear quadratic Gauss (LQG) methods of control in case of incomplete measurements of the state of the system.

Design/methodology/approach

The flexible wing with nonlinear aileron with freeplay is treated as a plant-controller system with H_∞ and LQG controllers used to suppress the aeroelastic vibrations. The simulation approach was used for analyzing the impact of completeness of measurements on the efficiency and robustness of the controllers.

Findings

The analysis shows that the H_∞ method can be effectively used for suppression of nonlinear aeroelastic vibrations of aileron, although its efficiency depends essentially on completeness and types of measurements. The LQG method is less effective, but it is also able to prevent aileron vibrations by reducing their amplitudes to acceptable, safe level.

Research limitations/implications

Only numerical analysis was carried out for the problem described; thus, the proposed solution is of theoretical value at this stage of analysis, and its application to the real suppression of aeroelastic vibrations requires further research.

Practical implications

The work presents a potentially useful solution to the problem of interest and results are a theoretical basis for further research.

Social implications

This work may lead to a hot debate on the advantages and drawbacks of the active suppression of vibrations in the aeroelasticians community.

Originality/value

The work raises the important questions of practical stabilizability of the nonlinear aeroelastic systems, their dependence on completeness and types of measurements and robustness of the controllers.

Citation

Dul, F. (2018), "Active suppression of freeplay aeroelastic vibrations of ailerons by robust control methods with incomplete measurements", Aircraft Engineering and Aerospace Technology, Vol. 90 No. 4, pp. 688-698. https://doi.org/10.1108/AEAT-11-2016-0215