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Indexed by:期刊论文

Date of Publication:2015-04-01

Journal:AEROSPACE SCIENCE AND TECHNOLOGY

Included Journals:SCIE、EI

Volume:42

Page Number:384-391

ISSN No.:1270-9638

Key Words:Rotating triangular tethered satellite formation; Nonlinear coupled dynamics; Dynamic simulation; Libration point

Abstract:The nonlinear coupled dynamics of a rotating triangular tethered satellite formation near libration points is presented. Based on Hill's approximation, the dynamical formulation for a rotating triangular tethered system near libration points is developed. The formulation comprises a set of strong nonlinear coupled equations. Numerical simulations using the full nonlinear and time-varying motion equations are performed for the station-keeping stages. The dynamic characteristics of the triangular tethered formation are analyzed. The numerical results demonstrate that the rotation rate has a significant impact on the stability of the system, whereas the orbital amplitude has a moderate impact on the stability of the systern. Tether length has little effect on the motion of the system's center of mass. It can be served as a basis to solve the problem of rotating triangular tethered systems in any arbitrary plane. (C) 2015 Elsevier Masson SAS. All rights reserved.