Dynamics of a space vehicle with elastic deploying tether

被引：10

作者：

Danilin, AN ^{[1
]}

Grishanina, TV ^{[1
]}

Shklyarchuk, FN ^{[1
]}

Buzlaev, DV ^{[1
]}

机构：

[1] TESIS Co, Moscow State Aviat Inst, Moscow, Russia

来源：

COMPUTERS & STRUCTURES | 1999年 / 72卷 / 1-3期

基金：

俄罗斯基础研究基金会;

关键词：

D O I：

10.1016/S0045-7949(99)00039-5

中图分类号：

TP39 [计算机的应用];

学科分类号：

081203 ; 0835 ;

摘要：

Equations of spatial motion of a space vehicle with an elastic deploying tether in the central gravitational field are obtained using for the tether a discrete model of concentrated masses connected by rectilinear massless extensible segments. Two examples are considered with the purpose to estimate the accuracy of the mathematical model and the numerical integration and to demonstrate the application of this model for solving highly nonlinear dynamic problems of variable systems. (C) 1999 Elsevier Science Ltd. All rights reserved.

引用

页码：141 / 147

页数：7