In this paper, the problem of attitude stabilization control of spacecraft under angular velocity
constraint is investigated. A state-constrained finite-time attitude control scheme is designed …

This article proposes a neural‐network‐based adaptive finite‐time output constraint control
scheme for attitude stabilization of rigid spacecrafts. First, a novel singularity‐free terminal …

In this article, a robust continuous controller is investigated to solve the global finite-time
attitude stabilization problem of rigid spacecraft system subject to multiple disturbances. The …

A finite-time attitude tracking control scheme is proposed for spacecraft using terminal
sliding mode and Chebyshev neural network (NN)(CNN). The four-parameter …

This article investigates the finite-time attitude tracking control problem of spacecraft with
angular velocity sensor failures and actuator saturation. A model-free angular velocity …

The performance of attitude stabilization control algorithms for rigid spacecraft can be limited
by disturbances. In this paper, the global finite-time attitude stabilization problem with …

In this paper, the control Lyapunov function (CLF) approach is adopted to investigate the
finite‐time attitude control of rigid spacecraft subject to parameter uncertainty and external …

This paper investigates the robust tracking control problem for spacecraft attitude
maneuvering with prescribed performance. Firstly, a control scheme is studied based on a …

In this paper, the problem of finite-time attitude-tracking control for a rigid spacecraft is
addressed. Uncertainties including unknown inertial parameters, external disturbances …

This paper investigates the attitude tracking problem of a rigid spacecraft using
contemporary predefined-time stability theory. To this end, the relative attitude kinematic and …