DLR@Uni Projekt Supercooled Large Droplet Icing (SuLaDI) – Methoden und Ansätze zur Erkennung von Vereisungseffekten am Flugzeug

Abstract

This report contains an overview about different concepts to detect the icing influence on aircraft. The work was part of the DLR@Uni project SuLaDI and contains for example the application of different system identification tools to detect the icing influence as well as the design of new optimal excitation maneuvers. Moreover, a novel methodology was developed to detect a flight performance degradation, which normally occurs in combination with aircraft icing. Furthermore, a way to determine an asymmetrical ice accretion is proposed. This report is a summary of various papers published within the SuLaDI project.