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

发布者:孙加亮发布时间:2020-07-31浏览次数:384

计及弯折波的舰载机拦阻过程控制

张萍,金栋平

 

摘要:本文计入弯折波,用PID控制方法研究了舰载机拦阻着舰过程中的动力学问题。鉴于弯折波在甲板滑轮与钩索啮合点之间反复传播的复杂性,首先不考虑弯折波,以液压阻尼力作为控制输入建立系统非线性动力学模型,按照尽可能使拦阻钩载保持常数这一要求,用最优控制方法获得了一组理想轨迹。然后,用PID控制方法进行跟踪控制,跟踪过程中采用了离散的弯折波模型。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,这与美军标MIL-STD-2066中的实验结果一致。

关键词:拦阻索;弯折波;动力学;PID控制;跟踪轨迹

 

Carrier Aircraft Arresting System Control Considering Kink-Wave

Ping Zhang, Dongping Jin

 

AbstractTaking kink-wave into account, the dynamic response of carrier aircraft during an arrested landing was studied by using PID control method. As it is a complex process of kink wave propagating repeatedly between the deck sheave and the hook, the nonlinear continuous mathematical model without regard to kink-wave was established, in which considering the hydraulic damping force as an input. Then, a set of ideal trajectory was found with optimal control method to make the hook load a constant as much as possible. Afterwards, the ideal response trajectory was tracked through using PID control method. During the tracking process, a discrete kink-wave model was used. The result shows that when taking kink-wave into account, the hook load will vibrate at the initial period of the arresting process, which is consistent with the experimental result of the American military standard MIL-STD-2066.

Keywordarresting cable; kink wave; dynamics; PID control; tracking trajectory

 

原文链接:http://hkxb.buaa.edu.cn/CN/abstract/abstract14137.shtml