计及弯折波的舰载机拦阻过程控制

doi:CNKI:11-1929/V.20110511.1349.003

固体力学与飞行器总体设计

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计及弯折波的舰载机拦阻过程控制

张萍, 金栋平

南京航空航天大学振动工程研究所, 机械结构强度与振动国家重点实验室, 江苏南京 210016

收稿日期:2011-03-07 修回日期:2011-04-07 出版日期:2011-11-25 发布日期:2011-11-24
通讯作者: 金栋平 E-mail:jindp@nuaa.edu.cn
作者简介:张萍(1986- ) 女,硕士研究生。主要研究方向:非线性动力学与控制。 Tel: 025-84891672 Email: crystal_zp@126.com 金栋平(1964- ) 男,博士,教授,博士生导师。主要研究方向:动力学与控制。 Tel: 025-84890251 E-mail: jindp@nuaa.edu.cn
基金资助:
长江学者和创新团队发展计划(IRT0968)

Control of Arresting Process for Carrier Aircraft Considering Kink-wave

ZHANG Ping, JIN Dongping

State Key Laboratory of Strength and Vibration for Mechanical Structures, Institute of Vibration Engineering Research, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China

Received:2011-03-07 Revised:2011-04-07 Online:2011-11-25 Published:2011-11-24

摘要/Abstract

摘要： 为验证拦阻索中应力的传播对拦阻过程的影响,研究了计及弯折波的舰载机拦阻过程的比例-积分-微分(PID)控制问题。先以液压阻尼力作为拦阻过程的控制输入建立了无弯折波的理想拦阻过程动力学模型,再依据拦阻过程中需要保持拦阻钩载为常值的要求,借助最优控制方法获得了一组理想轨迹。然后详细分析了拦阻索中弯折波在甲板滑轮与钩-索啮合点间的传播特征,获得了离散的弯折波模型,并将之应用于拦阻过程的PID跟踪控制中。结果表明,弯折波的计入,会使拦阻钩载在拦阻初期出现波动效应,这一现象与美国军用标准MIL-STD-2066中实验得到的钩载随行程变化规律一致。

关键词: 拦阻索, 弯折波, 动力学, PID控制, 跟踪轨迹

Abstract: To validate the influence of the stress wave propagation on the arresting process, this paper presents a study of the proportion-integral-differential (PID) control of the arresting process during carrier aircraft landing with consideration of the kink-wave that travels along the arresting cable. Taking the hydraulic damping force as a control input for the arresting process, a dynamic model for an ideal arrestment without the kink-wave is first established. Based on the constant hook load condition during the arresting process, a set of ideal trajectories is obtained with an optimal control method. Afterwards, the propagation characteristics of the kink-wave that travels between the deck sheave and the hook are analyzed. Then a discrete kink-wave model is obtained and applied to the PID control of the arresting process in tracking an ideal trajectory. The result shows that when the kink-wave is taken into consideration, the hook load will vibrate at the initial period of the arresting process, which is consistent with the experimental result of American military standard MIL-STD-2066.

Key words: arresting cable, kink-wave, dynamics, PID control, tracking trajectory

中图分类号:

V249

张萍, 金栋平. 计及弯折波的舰载机拦阻过程控制[J]. 航空学报, 2011, 32(11): 2008-2015.

ZHANG Ping, JIN Dongping. Control of Arresting Process for Carrier Aircraft Considering Kink-wave[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2011, 32(11): 2008-2015.

参考文献

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[11] 张澎森, 金栋平. 飞机拦阻过程的非线性最优控制[J]. 航空学报, 2009, 30(5): 849-854. Zhang Shusen, Jin Dongping. Nonlinear optimal control of aircraft arresting process[J]. Acta Aeronautica et Astronautica Sinica, 2009, 30(5): 849-854. (in Chinese)

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E-mail：hkxb@buaa.edu.cn

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主管单位：中国科学技术协会主办单位：中国航空学会北京航空航天大学

计及弯折波的舰载机拦阻过程控制

Control of Arresting Process for Carrier Aircraft Considering Kink-wave

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