Abstract Space missions to Near Rectilinear Halo Orbits (NRHOs) in the Earth–Moon system
are upcoming. A rendezvous technique in cislunar space is proposed in this investigation …

The autonomous ship landing control issue of multi-rotor Unmanned Aerial Vehicles (UAVs)
is investigated. To achieve the ship landing operation efficiently and precisely, a novel …

Recent studies highlighted the benefits of a support infrastructure located in Cislunar
environment, which would ease the design of forthcoming space missions with a favorable …

Predicting the attitude of spacecraft traveling within the Cislunar region is crucial to ensure
the success of future missions planned within that realm of space. To consider the coupled …

A novel, compact formalism of rigid body motion dynamics is presented in a general
reference frame based on the geometric mechanics framework. This formalism, proposed on …

Space missions to Near Rectilinear Halo Orbits (NRHOs) in the Earth-Moon system are
upcoming. A rendezvous technique in the cislunar space is proposed in this investigation …

It is crucial to be able to predict the attitude of spacecraft to guarantee mission success
within the Cislunar realm. To that end, the orbit/attitude coupling for the full N-body problem …

A compact formalism for rigid body motion dynamics is presented in a general reference
frame based on geometric mechanics. This formalism, proposed on the special Euclidean …

Interactions of the orbital motion on attitude dynamics of the gyrostat satellite are considered
in this paper. The mathematical model is derived using the Hamiltonian method for the spin …

Simultaneous tracking of orbit and attitude in multibody systems is essential for accurately
understanding motion. The cislunar region is effectively modeled using the circular restricted …