Nonlinear resonant analysis of space tethered satellite system in elliptical orbits

被引：4
|
作者：
Pang, Zhaojun [1 ]
Wen, Hao [2 ]
Rui, Xiaoting [3 ]
Du, Zhonghua [4 ]
机构：
[1] Nanjing Univ Sci & Technol, Sch Mech Engn, Inst Launch Dynam, Nanjing 210094, Peoples R China
[2] Nanjing Univ Aeronaut & Astronaut, State Key Lab Mech & Control Mech Struct, Nanjing 210016, Peoples R China
[3] Nanjing Univ Sci & Technol, Inst Launch Dynam, Nanjing 210094, Peoples R China
[4] Nanjing Univ Sci & Technol, Sch Mech Engn, Nanjing 210094, Peoples R China
来源：
ACTA ASTRONAUTICA | 2021年 / 182卷
基金：
中国国家自然科学基金;
关键词：
Tethered satellite; Resonance; Steady-state solutions; Bifurcation; Perturbation analysis; LIBRATION CONTROL; PERIODIC-SOLUTIONS; TENSION CONTROL; SUPPRESSION; STABILITY; DYNAMICS;
D O I：
10.1016/j.actaastro.2021.02.016
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
The nonlinear resonant motions of a tethered satellite system (TSS) in elliptical orbits are studied in this paper. The mathematical model of the system was derived using Lagrange's equations and an analysis of the parametric domain of the resonance was performed. It was revealed that internal resonance or combination resonance could occur in the system, but they did not occur simultaneously. The steady-state solutions of the system under combination resonance and internal resonance were analytically analyzed using the multiple scales method. The results showed that the steady-state solutions of the combination resonance and internal resonance had different bifurcation characteristics. Finally, the Poincare maps was employed to verify the analytical results.
引用
收藏
页码：264 / 273
页数：10
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