This paper investigates a new Agile Earth Observation Satellite (AEOS) mission planning
algorithm. This new developed algorithm is based on Modified Mixed-Integer Linear …

This paper deals with the problem of spacecraft time-optimal reorientation maneuvers under
boundaries and path constraints. The minimum time solution with keep-out constraints is …

The nanosatellite reorientation maneuver is one of the important elements of achieving the
mission goal if it is required to ensure the transfer of the nanosatellite axes from the initial to …

The spacecraft reorientation is a common task in many space missions. With multiple
pointing constraints, it is greatly difficult to solve the constrained spacecraft reorientation …

This paper proposes a novel feedback control law for spacecraft to deal with attitude
constraint, input saturation, and stochastic disturbance during the attitude reorientation …

Spacecraft are required to achieve fast attitude reorientation in many space missions.
However, the attitude maneuver will be limited by the bounded and pointing constraints. The …

CONSTRAINTS in a spacecraft's orientation often present chal-lenges in space missions, as
they make maneuvering a spacecraft a nontrivial problem. These hard orientation …

This paper addresses the time-optimal roto-translational orbital rendezvous maneuver for an
inertially asymmetric rigid spacecraft in an all-thrusters configuration. To begin with, the …

Lunar Reconnaissance Orbiter (LRO) was launched in 2009 to study and map the Moon and
is now completing its fifth extended science mission. The LRO (see) hosts a payload of …

This article investigates the spacecraft attitude reorientation control problem in the presence
of attitude constraint, actuator saturation, parametric uncertainty, and external disturbance …