Pitch Control by LQR for Fixed Wing Aircraft During Microburst Encounter

Autor: Ayyildiz, Sukru, Yazici, Hakan

Publikováno v: Proceeding Book of 5th International Conference on Advances in Mechanical Engineering: ICAME 2019 (pp.2297-2306). Istanbul, Turkey. ISBN 978-605-9546-16-4

In this study, a linear mathematical model representing longitudinal flight dynamics of an airplane is developed and responses of the aircraft during a microburst encounter are investigated. The effects of microburst that are acting on the aircraft a

Externí odkaz: http://arxiv.org/abs/2006.09942