甄子洋

教授

教授

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所在单位:自动化学院

学历:南京航空航天大学

办公地点:通信地址:南京市江宁区将军大道29号 南航自动化学院 邮编:211106

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Modeling, control design, and influence analysis of catapult-assisted take-off process for carrier-based aircrafts

发布时间:2020-03-23 点击次数:

所属单位:自动化学院
发表刊物:Proc. Inst. Mech. Eng. Part G J. Aerosp. Eng.
摘要:This paper addresses the problems of modeling, control design, and influence analysis of the steam catapult-assisted take-off process of the carrier-based aircrafts. The mathematical models of the carrier-based aircraft, steam catapult, landing gears, and the environmental factors including deck motion and bow airflow have been established to express the aircraft dynamics in the take-off process. An engineering method based automatic flight control system has been designed, which is divided into the longitudinal channel and lateral channel. The influences of the preset control surface, ship deck motion, ship bow airflow, and automatic flight control system system are tested by a series of simulations. The simulation results show that the elevator angle preset is necessary in the stage of accelerated running on the ship deck and the deck motion is the most important factor for safe take-off, while the ship bow airflow is beneficial for climbing up of the aircraft. The automatic flight control system gives the guarantee of safety and performance in the take-off process of the carrier-based aircraft. © IMechE 2017.
ISSN号:0954-4100
是否译文:
发表时间:2018-10-01
合写作者:江驹,王新华,Li, Kangwei
第一作者:甄子洋
通讯作者:甄子洋