Show simple item record

contributor authorRong, Bao
contributor authorRui, Xiaoting
contributor authorTao, Ling
date accessioned2017-05-09T00:56:01Z
date available2017-05-09T00:56:01Z
date issued2013
identifier issn0021-8936
identifier otherjam_80_1_011008.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/150783
description abstractIn many industrial applications, complex mechanical systems can often be described by multibody systems (MBS) that interact with electrical, flowing, elastic structures, and other subsystems. Efficient, precise dynamic analysis for such coupled mechanical systems has become a research focus in the field of MBS dynamics. In this paper, a coupled selfpropelled artillery system (SPAS) is examined as an example, and the discrete time transfer matrix method of MBS and multirate time integration algorithm are used to study the dynamics and cosimulation of coupled mechanical systems. The global error and computational stability of the proposed method are discussed. Finally, the dynamic simulation of a SPAS is given to validate the method. This method does not need the global dynamic equations and has a loworder system matrix, and, therefore, exhibits high computational efficiency. The proposed method has advantages for dynamic design of complex mechanical systems and can be extended to other coupled systems in a straightforward manner.
publisherThe American Society of Mechanical Engineers (ASME)
titleDiscrete Time Transfer Matrix Method for Launch Dynamics Modeling and Cosimulation of Self Propelled Artillery System
typeJournal Paper
journal volume80
journal issue1
journal titleJournal of Applied Mechanics
identifier doi10.1115/1.4006869
journal fristpage11008
journal lastpage11008
identifier eissn1528-9036
treeJournal of Applied Mechanics:;2013:;volume( 080 ):;issue: 001
contenttypeFulltext


Files in this item

Thumbnail

This item appears in the following Collection(s)

Show simple item record