Adaptive and quasi-sliding control of shimmy in landing gears
DA Burbano-L, M Coraggio… - 2018 European …, 2018 - ieeexplore.ieee.org
2018 European Control Conference (ECC), 2018•ieeexplore.ieee.org
Shimmy is a dangerous phenomenon that occurs when aircraft's nose landing gears
oscillate in a rapid and uncontrollable fashion. In this paper, we propose the use of two
nonlinear control approaches (zero average control and model reference adaptive control
based on minimal control synthesis) as simple yet effective strategies to suppress undesired
oscillations, even in the presence of uncertainties and partial state measurements.
Numerical results are presented to validate the proposed control approaches.
oscillate in a rapid and uncontrollable fashion. In this paper, we propose the use of two
nonlinear control approaches (zero average control and model reference adaptive control
based on minimal control synthesis) as simple yet effective strategies to suppress undesired
oscillations, even in the presence of uncertainties and partial state measurements.
Numerical results are presented to validate the proposed control approaches.
Shimmy is a dangerous phenomenon that occurs when aircraft's nose landing gears oscillate in a rapid and uncontrollable fashion. In this paper, we propose the use of two nonlinear control approaches (zero average control and model reference adaptive control based on minimal control synthesis) as simple yet effective strategies to suppress undesired oscillations, even in the presence of uncertainties and partial state measurements. Numerical results are presented to validate the proposed control approaches.
ieeexplore.ieee.org
以上显示的是最相近的搜索结果。 查看全部搜索结果