Newton-Euler equations of multibody systems with changing structures for space applications

被引：18

作者：

Aslanov, Vladimir ^{[1
]}

Kruglov, Genrih ^{[1
]}

Yudintsev, Vadim ^{[1
]}

机构：

[1] Korolev Samara State Aerosp Univ, Samara, Russia

来源：

ACTA ASTRONAUTICA | 2011年 / 68卷 / 11-12期

基金：

俄罗斯基础研究基金会;

关键词：

Multibody systems; Variable structure; Joint; Newton Euler equation; Constraints; Rigid body; DYNAMICS;

D O I：

10.1016/j.actaastro.2010.11.013

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

Multibody systems with changing structure are considered. These systems have stages in their motion that distinct from each other by degree of freedom (DOE), joint connection structure and joint types. These mechanical systems are common in space application e.g. separation subsystems. Single coordinate set is used to formulate Newton-Euler equations of motion at each stage. Proposed equation form simplifies equations building process for certain stages and whole motion. Numerical experiment was carried out using proposed method. (C) 2010 Elsevier Ltd. All rights reserved.

引用

页码：2080 / 2087

页数：8

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