There are approximately 2900 active space objects cataloged, and the number will increase
continually in future. All these space objects may maneuver for some purpose occasionally …

In the present work, the problem of frozen orbits of a charged satellite around the Earth is
treated. The geopotential is considered as oblate body up to J 6 zonal harmonics. The first …

In this paper, the orbital motion of an electrically charged spacecraft in the gravitational and
magnetic fields of the Earth is investigated. The “direct magnetic dipole” is considered as a …

Attitude stabilization of a charged rigid spacecraft in Low Earth Orbit using torques due to
Lorentz force in pitch and roll directions is considered. A spacecraft that generates an …

The objective of this research is to address the issue of frozen orbits in charged satellites by
incorporating geopotential zonal harmonics up to J6 and the initial tesseral harmonics. The …

In a geocentric kinematically rotating ecliptical coordinate system in geodesic motion
through the deformed spacetime of the Sun, both the longitude of the ascending node and …

In this work, the perturbations in all orbital elements due to the motion of the charged
satellites in the Earth's magnetic field using Lagrange's planetary equations are solved …

A satellite with a system of three electrostatic radiation protection (ERP) screens is under
consideration. The screens are constructed as electrostatically charged toroidal shields with …

The inclination I of an Earth's satellite in polar orbit undergoes a secular De Sitter precession
of-\, 7.6-7.6 milliarcseconds per year for a suitable choice of the initial value of its non …

The electrostatic charge became a possible method to control both orbital and attitude
motion without fuel consumption or reduce the fuel cost. This study needs to install an ion …