Sedlmair, NicolasNicolasSedlmairTheis, JulianJulianTheisThielecke, FrankFrankThielecke2020-01-142020-01-142019-11-25IFAC-PapersOnLine 12 (52): 316-321 (2019)http://hdl.handle.net/11420/4365A multivariable flight control law for automatic landing of an unmanned aircraft with tailwheel gear configuration is developed in this paper. The control law is obtained using H∞-synthesis and implemented in a differential form to facilitate bumpless transfer, i.e. correct initialization when switching control laws, and anti-windup compensation. The controller is evaluated using a validated high-fidelity model of the aircraft and Monte-Carlo simulations.en2405-8963201912316321Elsevierhttps://creativecommons.org/licenses/by-nc-nd/4.0/Flight controlMultivariable control systemsRobust control applicationsTechnikJournal Article10.15480/882.347010.1016/j.ifacol.2019.11.26210.15480/882.3470Other