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A Semi-Active Controller for an Aircraft Landing Gear Equipped with Magnetorheological Damper
- Source :
- Applied Mechanics and Materials. 894:29-33
- Publication Year :
- 2019
- Publisher :
- Trans Tech Publications, Ltd., 2019.
-
Abstract
- The magnetorheological (MR) damper is the newest approach to replace the traditional passive damper which cannot change their dynamics in response to different operating conditions of the aircraft landing gear. This paper presents the simulation study of a semi-active controller for a landing gear equipped MR damper. Furthermore, a new method combined skyhook control with force control, called hybrid control, is developed to improve the performance of the MR damper landing gear. Finally, the numerical simulation result of the landing gear using SIMSCAPE-Simulink is discussed.
- Subjects :
- Aircraft landing
0209 industrial biotechnology
Semi active
020901 industrial engineering & automation
Computer science
Control theory
0202 electrical engineering, electronic engineering, information engineering
020201 artificial intelligence & image processing
02 engineering and technology
General Medicine
Magnetorheological damper
Automotive engineering
Landing gear
Subjects
Details
- ISSN :
- 16627482
- Volume :
- 894
- Database :
- OpenAIRE
- Journal :
- Applied Mechanics and Materials
- Accession number :
- edsair.doi...........29619f952abe15f119904b598fe84fd9