BACKSTEPPING is a popular nonlinear control design tech-nique [1, 2]. It hinges on using a
part of the system states as virtual controls to control the other states. Generating a family of …

A practical solution is presented to the problem of fault tolerant attitude stabilization for a
rigid spacecraft by using feedback from attitude orientation only. The attitude system …

This paper addresses the finite‐time formation tracking problem for multiple vehicles with
dynamics model on SE (3)(the specific Euclidean group of rigid body motions), under the …

We propose a central synergistic hybrid approach for global exponential stabilization on the
Special Orthogonal group SO (3). We introduce a new switching concept relying on a central …

This article presents a 6-DOF attitude-orbit synchronous control problem for the space
circumnavigation (SCN) mission with parameter uncertainties, time-varying uncertainties …

The problem of fault tolerant attitude stabilization with finite‐time convergence is
investigated for spacecraft with redundant actuators. On the basis of the sliding mode control …

We present a solution to the problem of tracking relative rotation in a leader–follower
spacecraft formation using feedback from relative attitude only. The controller incorporates …

Plug-and-play technology is an important direction for future development of spacecraft and
how to design controllers with less communication burden and satisfactory performance is of …

In this paper, we present an algorithm for planning and control of legged robot locomotion.
Given the desired contact sequence, this method generates gaits and dynamic motions for …

Most existing methods for satellite attitude control assume that full knowledge of satellite
attitude is available by algebraic manipulation of at least two vector measurements from …