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Modeling, analysis and non-linear control of a novel pneumatic semi-active vibration isolator: A concept validation study.

机译:新型气动半主动隔振器的建模,分析和非线性控制:概念验证研究。

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摘要

Advanced suspension systems play a crucial role in the performance of vehicles. The essential problem in designing a vibration isolator for a system comprises of controlling the relative motion between the suspended mass and the base due to stroke limitations, while attenuating the vibration transmitted to the mass from the base. These two requirements being conflicting in nature results in a compromised suspension design when purely passive isolation technologies are employed. Active vibration isolation systems which totally eliminated this compromise have cost, maintenance and reliability issues precluding them from being used in many applications. Semi-active technologies on the other hand provide feasible alternative to the active systems, but employ oil based dampers, which deteriorates the performance over a wide range of operating regime.;The thesis presents a novel semi-active pneumatic vibration isolation technology, which is capable of alleviating the drawbacks of both the contemporary active and the semi-active systems currently being researched. The pneumatic system proposed was shown to have the capability to continuously alter its natural frequency and damping characteristics (CVNFD) without needing either a hydraulic actuator or oil based variable damping device. The computational study based on the non-linear mathematical model developed showed the CVNFD behavior of the pneumatic system and the experiments conducted on the research test-rig corroborated the result.;Two non-linear control schemes in the form of Skyhook control and sliding mode control were used to synthesize controllers for the pneumatic system. A modified skyhook control was derived and implemented on the pneumatic system. The performance of this controller was shown to rival that obtained for a conventional semi-active system using the Magneto-Rhealogical (MR) damper and controlled by skyhook control. A more advanced non-linear robust control scheme called sliding mode control was used for the second controller design. The controller was synthesized using the sliding mode control theory applied to the theory of model-matching. Lyapunov stability analysis was applied and the sliding mode controller was modified to guarantee global asymptotic stability. It was demonstrated computationally as well as experimentally that by suitably choosing the several controller design-parameters, the skyhook based sliding mode controller can recover the performance lost by implementing the model independent skyhook law.;In summary, the research conducted in this thesis demonstrated the availability and feasibility of a new and novel semi-active pneumatic vibration isolation technology that can replace and/or enhance the performance of contemporary passive and semi-active systems.
机译:先进的悬架系统在车辆性能中起着至关重要的作用。设计用于系统的隔振器的基本问题包括:由于行程限制而控制悬吊质量块和基座之间的相对运动,同时减弱从基座传递到质量块的振动。当采用纯被动隔离技术时,这两个要求本质上会产生冲突,从而导致悬架设计受损。完全消除了这种折衷的有源振动隔离系统存在成本,维护和可靠性问题,因此无法在许多应用中使用。另一方面,半主动技术为主动系统提供了可行的替代方案,但采用了油基阻尼器,这会在广泛的工作范围内降低性能。能够减轻目前正在研究的现代主动和半主动系统的弊端。所提出的气动系统被证明具有连续改变其固有频率和阻尼特性(CVNFD)的能力,而无需液压致动器或油基可变阻尼装置。基于所开发的非线性数学模型的计算研究表明了气动系统的CVNFD行为,并且在研究试验台上进行的实验证实了这一结果。;两种形式为Skyhook控制和滑模控制的非线性控制方案控制器用于合成气动系统的控制器。派生出改进的天钩控制装置,并在气动系统上实施。事实证明,该控制器的性能可与使用磁流变(MR)阻尼器并由天钩控制的传统半主动系统媲美。在第二个控制器设计中使用了一种更先进的称为滑模控制的非线性鲁棒控制方案。控制器是采用滑模控制理论应用于模型匹配理论而合成的。应用了Lyapunov稳定性分析,并修改了滑模控制器以确保全局渐近稳定性。通过计算和实验证明,通过适当选择几个控制器设计参数,基于天钩的滑模控制器可以通过实现与模型无关的天钩定律来恢复损失的性能。可以替代和/或增强当代被动和半主动系统性能的新型半主动气动隔振技术的可用性和可行性。

著录项

  • 作者

    Porumamilla, Hemanth.;

  • 作者单位

    Iowa State University.;

  • 授予单位 Iowa State University.;
  • 学科 Engineering Mechanical.
  • 学位 Ph.D.
  • 年度 2007
  • 页码 159 p.
  • 总页数 159
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

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