In this work, a saturated explicit reference governor (ERG) control scheme is proposed to
achieve attitude reorientation maneuver in the presence of pointing constraints and input …

This article investigates the autonomous spacecraft rendezvous and docking problem in the
presence of space obstacle, path constraints, and thrust limitation constraint. By introducing …

Control engineering has made significant progress in addressing various challenges for real-
world applications. For the next stage of robotics automation, it is necessary to guarantee …

This paper presents a provably safe method for constrained reorientation of a spacecraft in
the presence of input constraints, bounded disturbances, and fixed frequency zero-order …

This paper addresses the attitude reorientation problem under the pointing-constraint zone,
angular velocity limits, and actuator constraints. The ERG-based control scheme is designed …

This paper experimentally validates the invariant-set motion planner (ISMP) for the
spacecraft attitude motion planning problem. Three novel results are presented that enable …

This paper introduces an optimal trajectory planner for spacecraft rest-to-rest attitude
transfers subject to input saturation, angular velocity, and nonconvex exclusion cone …

This paper focuses on the constrained attitude control of a rigid body. We propose an
Explicit Reference Governor (ERG) specifically designed to handle constraints on SO (3) …

This article studies the appointed-time attitude tracking control of the spacecraft on the
special orthogonal group, with the attitude forbidden zone, the parameter uncertainties, and …

The action governor is an add-on scheme to a nominal control loop that monitors and
adjusts the control actions to enforce safety specifications expressed as pointwise-in-time …