The design of complex aerospace systems is a multidisciplinary design optimization (MDO)
problem involving the interaction of multiple disciplines. However, because of the necessity …

With the escalating frequency of space activities, particularly the launch of constellation
satellites, the amount of space debris experienced gradually increases, posing threats to the …

Abstract Objects in Low-Earth Orbit (LEO) experience a range of environmental conditions
that influence their trajectories. Aside from gravitational effects and solar radiation pressure …

Abstract 50,000+ satellites are scheduled for launch by 2030, bringing both massive
opportunities and equally massive challenges. Key among these challenges is the ability to …

International guidelines recommend removing any artificial body in Low Earth Orbit (LEO)
within 25 years from mission completion. Among disposal strategies, electrodynamic tethers …

In order to help control the spread of space debris and junk, deorbit sail devices have been
used for deorbiting techniques; however, this approach is still considered risky due to …

Relative motion control problem for capturing the tumbling space debris object is
considered. Onboard thrusters and reaction wheels are used as actuators. The nonlinear …

The rapid increase in the number of space debris represents a substantial threat to the
sustained viability of space operations. Monitoring these debris is critical for space …

The growing number of satellites operating in LEO highlights the necessity for a better
understanding of ionospheric aerodynamics to mitigate collision risks, ensure in-orbit safety …

Predicting the ionospheric aerodynamic forces acting on a satellite in low Earth orbit (LEO)
is critical both in terms of avoiding collisions with other satellites in this area as well as …