Approximate solutions for tethered satellite motion

Journal of Guidance, Control, and Dynamics

Volumn 24, Issue 4, 2001, Pages 746-754

  Cho, S ^a   Lovell, T A ^b   Cochran, J E ^b   Cicci, D A ^b  

^a Electronics and Telecommunications Research Institute (ETRI)   (South Korea)

^b AUBURN UNIVERSITY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

APPROXIMATION THEORY; EQUATIONS OF MOTION; MATHEMATICAL MODELS; ORBITS; PERTURBATION TECHNIQUES; SATELLITES; TETHERLINES;

ORBITAL MOTION; TETHERED SATELLITE SYSTEM;

SPACE FLIGHT;

EID: 0035394682     PISSN: 07315090     EISSN: None     Source Type: Journal    
DOI: 10.2514/2.4775     Document Type: Article

References (10)

1. Identification and orbit determination of tethered satellite system
2. On the information contained in the motion of one satellite of a two-satellite tethered system
3. Some approximations for the dynamics of spacecraft tethers
4. Dynamics analysis of electrodynamic satellite tethers equations of motion and numerical solution algorithms for the tether
5. Analysis of orbital motion of a tethered satellite system
6. Dynamics and orbit determination of tethered satellite systems