所属单位：自动化学院
发表刊物：Chinese Control Conf., CCC
摘要：This paper studies the automatic carrier landing control problem of unmanned aerial vehicle (UAV), by applying a model reference adaptive control (MRAC) scheme to deal with system uncertainties. Two key issues are solved for UAV carrier landing, including flight deck motion disturbance compensation and glide slope tracking control. An automatic carrier landing system (ACLS) for carrier-based UAV is developed, in which the flight control subsystem plays an important role. A state feedback for output tracking multivariable MRAC scheme is used to design the longitudinal flight controller and the lateral flight controller, which guarantees the arbitrary reference trajectory tracking. Simulation results demonstrate that the adaptive ACLS ensures the UAV asymptotically track the glide path even under the flight deck motion disturbance. © 2018 Technical Committee on Control Theory, Chinese Association of Automation.
ISSN号：1934-1768
是否译文：否
发表时间：2018-10-05
合写作者：Tao, Gang,江驹,杨柳庆
第一作者：甄子洋
通讯作者：甄子洋