This paper studies the dynamics of nanosatellite deorbit by a bare electrodynamic tether.
The orbital dynamics of the tethered nanosatellite is modeled in Gaussian perturbation …

This paper studies libration dynamics and stability of deorbiting nano-satellites by short and
bare electrodynamic tethers. A critical aspect of satellite deorbit by an electrodynamic tether …

This paper studies satellite deorbit using electrodynamic tether (EDT) propulsion. Gaussian
perturbation equations are used to model the orbital dynamics of EDT with environmental …

Electrodynamic tether systems orbiting the Earth are prone to libration instability because of
periodic changes in the geomagnetic field, plasma density, and lunisolar gravitational …

This paper studies the long term dynamics and optimal control of a nano-satellite deorbit by
a short electrodynamic tether. The long term deorbit process is discretized into intervals and …

This paper developed a high-fidelity dynamic model of flexible space tether systems by
considering the elastic, thermal, and electrical coupling effects on the dynamics and stability …

The paper investigates the elastic, thermal, and electrical coupling effects on the dynamics
and libration stability of flexible bare electrodynamic tethers in the end-of-mission satellite …

Tethered satellites have a vast potential for space applications. If the tether is conductive,
electrodynamic forces result from the motion of the conductive tether relative to the magnetic …

In the last decades, green deorbiting technologies have begun to be investigated and have
raised a great interest in the space community. Among the others, electrodynamic tethers …

This paper investigates spacecraft orbital boost maneuver by a fully insulated
electrodynamic tether using a coupled multiphysics dynamic model that considers electric …