Inspired by the integrated guidance and control design for endo-atmospheric aircraft, the
integrated position and attitude control of spacecraft has attracted increasing attention and …

An adaptive finite-time attitude and position coupled tracking controller for six-degree-of-
freedom (6-DOF) leader-following spacecraft formation is proposed in this paper. The …

By integrating the finite time control technique and finite-time disturbance observers
together, the finite-time three-dimensional path following control problem for small-scale …

This work deals with the development of a decentralized optimal control algorithm, along
with a robust observer, for the relative motion control of spacecraft in leader-follower based …

This paper considers the problem of finite-time disturbance observer (FTDO) design and the
problem of FTDO based finite-time control for systems subject to nonvanishing disturbances …

This paper is concerned with prescribed-time control for spacecraft formation flying. Firstly,
based on Lie group SE (3), the coupled 6-degrees-of-freedom kinematics and dynamics for …

This paper studies the prescribed-time spacecraft formation flying problem under known and
unknown external disturbance. The coupled 6-degrees-of-freedom relative kinematics and …

This paper considers the spacecraft formation flying (SFF) with a desired attitude. Two
control problems are studied. One is the formation control of multiple spacecraft and the …

The problem of controlling coupled six-degrees-of-freedom (6-DOF) relative motion of an
integrated-actuation spacecraft in the presence of actuator faults, and especially failures, is …

The integrated 6‐DOF orbit‐attitude dynamical modeling and control have shown great
importance in various missions, for example, formation flying and proximity operations. The …