Modeling and adaptive control of magneto-rheological buffer system for aircraft landing gear

Fu Li; Guan Wei; Wang Qi; Xu Xinhe

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Modeling and adaptive control of magneto-rheological buffer system for aircraft landing gear

机译：飞机起落架磁流变缓冲系统的建模与自适应控制

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The main advantages of magneto-rheological buffer system for aircraft landing gear are adjustable damping force, simple structure and independent of external energy. A kind of magneto-rheological damper structure for aircraft landing gear was presented in this paper. The state equation was established and the landing buffer system control strategy was designed based on self-made magneto-rheological landing impact platform. Integrating with model predictive control, a semi-active control method was studied and used it in realizing the adaptive magneto-rheological buffer system landing process. It has been proved in practice that the proposed control method fully considered the boundless of output damping force. The problem of balancing between landing and taxiing, which is caused by un-adjustable passive damping force in the working process of oleo-pneumatic buffer system, is solved.

机译：飞机起落架的磁流变缓冲系统的主要优点是阻尼力可调，结构简单且不受外部能量的影响。提出了一种飞机起落架的磁流变阻尼器结构。建立了状态方程，并基于自制的磁流变降落冲击平台设计了降落缓冲系统的控制策略。与模型预测控制相结合，研究了一种半主动控制方法，并将其用于实现自适应磁流变缓冲系统着陆过程。实践证明，提出的控制方法充分考虑了输出阻尼力的无限性。解决了油-气缓冲系统工作过程中由于被动阻尼力无法调节而引起的着陆与滑行之间的平衡问题。

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来源
《Applied Mathematical Modelling》 |2015年第9期|2509-2517|共9页
作者
Fu Li; Guan Wei; Wang Qi; Xu Xinhe;
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作者单位

Shenyang Aerospace University, Liaoning Shenyang 110136, China;

Shenyang Aerospace University, Liaoning Shenyang 110136, China;

Shenyang Aerospace University, Liaoning Shenyang 110136, China;

Northeastern University, Liaoning Shenyang 110104, China;

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收录信息美国《科学引文索引》(SCI);美国《工程索引》(EI);
原文格式 PDF
正文语种 eng
中图分类
关键词
Aircraft landing gear; Magneto-rheological buffer system; State equation; Adaptive control; Semi-active control;

机译：飞机起落架;磁流变缓冲系统;状态方程;自适应控制半主动控制;

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1. Modeling and Control of the Pulley Buffer System of Arresting Cable for Shipboard Aircraft Based on Magneto-Rheological Fluid [J] . FU Li, WEI Ying, ZHOU Yan-kai, 上海交通大学学报（英文版） . 2012,第005期
2. Landing efficiency control of a six degrees of freedom aircraft model with magneto-rheological dampers: Part 2-control simulation [J] . Byung-Hyuk Kang, Ji-Young Yoon, Gi-Woo Kim, Journal of intelligent material systems and structures . 2021,第12期

机译：磁力流变阻尼器六个自由飞机模型的着陆效率控制：第2部分控制模拟
3. Observer Based Optimal Vibration Control of a Full Aircraft System Having Active Landing Gears and Biodynamic Pilot Model [J] . Yazici Hakan, Sever Mert Shock and vibration . 2016,第PTa7期

机译：具有主动起落架和生物动力飞行员模型的全机系统基于观测器的最佳振动控制
4. Semi-active control of a landing gear system using magneto-rheological damper [C] . Y. J. Nam, M. K. Park, J. W. Choi, International Conference on Mechatronics and Information Technology . 2008

机译：磁流变阻尼器的着陆齿轮系统半主动控制
5. Advances in optimal active control techniques for aerospace systems; application to aircraft active landing gear. [D] . Vu, Khai Tran. 1989

机译：航空系统最佳主动控制技术的进展；应用于飞机主动起落架。
6. Control System for Vertical Take-Off and Landing Vehicle’s Adaptive Landing Based on Multi-Sensor Data Fusion [O] . Hongyan Tang, Dan Zhang, Zhongxue Gan 2020

机译：基于多传感器数据融合的垂直起飞和着陆车辆自适应降落控制系统
7. Intelligent Control Based on a Neural Network for Aircraft Landing Gear with a Magnetorheological Damper in Different Landing Scenarios [O] . Quoc Viet Luong, Dae-Sung Jang, Jai-Hyuk Hwang 2020

机译：基于不同着陆场景中磁流变阻尼器的飞机着陆齿轮神经网络的智能控制

Modeling and adaptive control of magneto-rheological buffer system for aircraft landing gear

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