Dynamics and control of the tethered satellite system in the presence of offsets

1987 ◽  
Vol 15 (12) ◽  
pp. 1053-1057 ◽  
Author(s):  
P.K. Lakshmanan ◽  
V.J. Modi ◽  
A.K. Misra
Keyword(s):  
Satellite System ◽  
Tethered Satellite ◽  
Tethered Satellite System ◽  
Dynamics And Control ◽  
And Control

scholarly journals Dynamics and Control of a Tethered Satellite System Based on the SDRE Method

2016 ◽  
Vol 2016 ◽  
pp. 1-16 ◽  
Author(s):  
Yong-Lin Kuo
Keyword(s):  
Nonlinear Dynamic ◽  
Equations Of Motion ◽  
Nonlinear Dynamic Analysis ◽  
Satellite System ◽  
Convergence Time ◽  
Tethered Satellite ◽  
Modeling And Control ◽  
Tethered Satellite System ◽  
Dynamics And Control ◽  
And Control

This paper presents the nonlinear dynamic modeling and control of a tethered satellite system (TSS), and the control strategy is based on the state-dependent Riccati equation (SDRE). The TSS is modeled by a two-piece dumbbell model, which leads to a set of five nonlinear coupled ordinary differential equations. Two sets of equations of motion are proposed, which are based on the first satellite and the mass center of the TSS. There are two reasons to formulate the two sets of equations. One is to facilitate their mutual comparison due to the complex formulations. The other is to provide them for different application situations. Based on the proposed models, the nonlinear dynamic analysis is performed by numerical simulations. Besides, to reduce the convergence time of the librations of the TSS, the SDRE control with a prescribed degree of stability is developed, and the illustrative examples validate the proposed approach.

scholarly journals Dynamics and Control of Tethered Satellite System in Elliptical Orbits under Resonances

2020 ◽  
Vol 2020 ◽  
pp. 1-12
Author(s):  
Zhaojun Pang ◽  
Zhonghua Du ◽  
Chun Cheng ◽  
Qingtao Wang
Keyword(s):  
Chaotic Motion ◽  
Satellite System ◽  
Internal Resonances ◽  
Tethered Satellite ◽  
Tethered Satellite System ◽  
Dynamics And Control ◽  
Elliptical Orbits ◽  
And Control ◽  
Stable Domains ◽  
Parameter Relations

This paper studies resonance motions of a tethered satellite system (TSS) in elliptical orbits. A perturbation analysis is carried out to obtain all possible resonance types and corresponding parameter relations, including internal resonances and parametrically excited resonances. Besides, a resonance parametric domain is given to provide a reference for the parameter design of the system. The bifurcation behaviors of the system under resonances are studied numerically. The results show that resonant cases more easily enter chaotic motion than nonresonant cases. The extended time-delay autosynchronization (ETDAS) method is applied to stabilize the chaotic motion to a periodic one. Stability analysis shows that the stable domains become smaller in resonance cases than in the nonresonance case. Finally, it is shown that the large amplitudes of periodic solutions under resonances are the main reason why the system is difficult to control.

Current Collection Model Characterizing Shuttle Charging During the Tethered Satellite System Missions

2000 ◽  
Vol 37 (2) ◽  
pp. 212-217 ◽  
Author(s):  
Victor M. Aguero ◽  
Brian E. Gilchrist ◽  
Scott D. Williams ◽  
William J. Burke ◽  
Linda Krause ◽  
...  
Keyword(s):  
Satellite System ◽  
Tethered Satellite ◽  
Tethered Satellite System ◽  
Current Collection

Dynamic analysis of a tethered satellite system with a moving mass

2013 ◽  
Vol 75 (1-2) ◽  
pp. 267-281 ◽  
Author(s):  
Wonyoung Jung ◽  
Andre P. Mazzoleni ◽  
Jintai Chung
Keyword(s):  
Dynamic Analysis ◽  
Satellite System ◽  
Moving Mass ◽  
Tethered Satellite ◽  
Tethered Satellite System
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