2026-04-17T06:17:29Zhttps://recercat.cat/oai/request

oai:recercat.cat:2117/133382025-07-17T05:48:50Zcom_2072_1033col_2072_452950

urn:hdl:2117/13338 Landing gear suspension control through adaptive backstepping techniques with H-infinity performance Zapateiro, Mauricio Pozo Montero, Francesc Rossell Garriga, Josep Maria Karimi, Hamid Reza Luo, Ningsu Àrees temàtiques de la UPC::Enginyeria mecànica::Mecànica::Vibracions mecàniques Àrees temàtiques de la UPC::Matemàtiques i estadística Vibration (Aeronautics) Damping (Mechanics) Vibració (Aeronàutica) Amortiment (Mecànica) Classificació AMS::93 Systems Theory; Control Landing gear suspension systems ful ll the tasks of absorbing the vertical energy of the touch-down as well as providing passenger and crew comfort with a smooth ground ride before take-o and after landing. They are also designed to have optimal performance in the case of a hard landing. In general, the tasks of aircraft landing gears are complex and sometimes lead to a number of contradictory requirements. Although there are existing modi cations of aircraft shock absorbers to reduce the problem, the basic design con ict between the requirements for landing and for rolling cannot be fully overcome by a passive suspension layout. Active and semiactive suspension techniques are a solution to this problem and are capable of reducing fuselage vibrations e ectively. In order to get satisfactory damping performance with active and semiactive devices, appropriate control laws must be employed. In this paper, we study the use of an adaptive backstepping control with H-infinity performance to cope with disturbances, uncertainties and nonlinearities, typical of suspension systems and damping devices. A comparison between active and semiactive strategies is provided through the analysis of simulation results Preprint 2011 Conference lecture http://www.ifac-papersonline.net/ http://www.ifac-papersonline.net/Detailed/49059.html Open Access