Suppression of Chaotic Motion of Tethered Satellite Systems Using Tether Length Control Article Swipe
Related Concepts
Satellite
Spacecraft
Base (topology)
Orbit (dynamics)
Aerospace engineering
Drag
Physics
Sun-synchronous orbit
Motion (physics)
Geodesy
Circular orbit
Classical mechanics
Mechanics
Geology
Engineering
Mathematics
Mathematical analysis
Geostationary orbit
Francisco Salazar
,
A. F. B. A. Prado
·
YOU?
·
· 2023
· Open Access
·
· DOI: https://doi.org/10.48550/arxiv.2307.12990
· OA: W4385291690
YOU?
·
· 2023
· Open Access
·
· DOI: https://doi.org/10.48550/arxiv.2307.12990
· OA: W4385291690
This study focuses on attitude and control motion of two bodies (a base-satellite and a sub-satellite) connected by an inextensible and massless tether in a circular orbit under the influence of the Earths gravitational force. The base-satellite is assumed to be far more heavier than the sub-satellite. In such cases, the base-satellite is regarded as the reference spacecraft. Because of the complexity of the problem, no thrusters on the sub-satellite are considered, and the effect of atmospheric drag, Earths oblateness, and electrodynamic force on the spacecraft are neglected.
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