Application of High-speed Solenoid Valve to the Semi-active Control of Landing Gear
Liu Hui,Gu Hongbin,Chen Dawei +2 more
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TLDR
In this paper, a nonlinear high-speed solenoid valve model is developed with the consideration of magnetic saturation characteristics and verified by test, according to the design rule of keeping the peak load as small as possible while absorbing the specified shock energy.About:
This article is published in Chinese Journal of Aeronautics.The article was published on 2008-06-01 and is currently open access. It has received 25 citations till now. The article focuses on the topics: Solenoid valve & Solenoid.read more
Citations
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TRIZ-Based Guidelines for Eco-Improvement
Davide Russo,Christian Spreafico +1 more
TL;DR: A rigorous ontology indicating how to apply a specific problem-solving strategy onto a specific part of the problem is proposed, trying to make the user aware of the environmental consequences of his design changes.
Journal ArticleDOI
Multi-domain modeling and simulation of proportional solenoid valve
TL;DR: In this paper, a multi-domain nonlinear dynamic model of a proportional solenoid valve was presented, where electro-magnetic, mechanical and fluid subsystems of the valve were investigated, including their interactions.
Journal ArticleDOI
Investigation on Electromagnetic Models of High-Speed Solenoid Valve for Common Rail Injector
TL;DR: Based on the electromagnetic transient coupling principle, an electromagnetic mathematical model of a high-speed solenoid valve (HSV) is developed in Fortran language that takes the saturation phenomena of the electromagnetic force into consideration as mentioned in this paper.
Journal ArticleDOI
Direct drive servo valve based on magnetostrictive actuator: Multi-coupled modeling and its compound control strategy
TL;DR: In this paper, a multi-coupled model of a direct drive servo valve driven by giant magnetostrictive actuator (GMM-DDV) is established with its constitute hysteresis studied based on Jiles-Atherton model.
Journal ArticleDOI
A critical review on the solenoid valve reliability, performance and remaining useful life including its industrial applications
S.V. Angadi,Robert L. Jackson +1 more
TL;DR: In this article , the vital operational characteristics such as reliability, performance and remaining useful life (RUL) pertaining to the electromagnetic solenoid valves (SVs), which govern their successful functioning and safe operation during service, are taken into account via a thorough review of the literature.
References
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Journal ArticleDOI
Semi‐Active versus Passive or Active Tuned Mass Dampers for Structural Control
TL;DR: In this article, a semi-active tuned mass damper (TMD) is proposed to control wind induced vibrations in tall buildings, which uses a small amount of external power to modulate the damping.
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Semi-Active Heave and Pitch Control for Ground Vehicles
TL;DR: In this paper, a model of a vehicle traversing a roadway is presented, which includes both the heave and pitch motions of the vehicle, and control strategies for the totally active case and vehicle isolation is demonstrated.
DissertationDOI
Integrated design process for the development of semi-active landing gears for transport aircraft
TL;DR: In this article, three control laws, a skyhook-type controller, a fuzzy-logic controller, and a state feedback controller are designed for the application of a semi-active suspension for an aircraft nose landing gear.
Journal ArticleDOI
Dynamic model of the plunger type solenoids at deenergizing state
TL;DR: By introducing appropriate assumptions, the author developed a set of equations which describe the deenergizing state of solenoids and perform test results satisfactorily and requires small amount of computer time to execute.
Journal ArticleDOI
GA-Based Model Predictive Control of Semi-Active Landing Gear
Dong-su Wu,Hong-bin Gu,Hui Liu +2 more
TL;DR: In this article, a nonlinear model predictive control algorithm (NMPC) for semi-active landing gears is developed, which uses GA as the optimization technique and chooses damping performance of landing gear at touch down to be the optimization object.