Due to the complexly natural attributes of technical systems, reality has been shown that
many systems could be modeled more precisely if they are modeled by using fractional …

This paper investigates the robust finite-time attitude tracking control problem for rigid
spacecraft considering the modeling uncertainty, external disturbance and actuator …

In this paper, the attitude tracking control for a spacecraft system based on a novel adaptive
integral-type terminal sliding mode fault-tolerant control strategy is investigated. First, a basic …

A sliding mode based finite-time control scheme is presented to address the problem of
attitude stabilization for rigid spacecraft in the presence of actuator fault and external …

A kind of non-contact vibration measurement method for a two-connected flexible
piezoelectric plate using laser sensors is proposed. Decoupling of the bending and torsional …

Most bilateral teleoperation researches focus on the system stability within time-delays.
However, practical teleoperation tasks require high performances besides system stability …

This paper investigates two finite-time controllers for the attitude tracking control of the
spacecraft based on the quaternion by terminal sliding mode control. Because quaternion is …

This paper provides a new solution for the finite‐time attitude maneuvers of rigid spacecraft.
Uncertainties involving unknown inertial parameters, external disturbances and actuator …

In this paper, a robust adaptive finite time sliding mode control method is proposed for the
attitude control of a rigid spacecraft. The proposed control method is derived using a novel …

A finite-time convergent sliding mode control (SMC) scheme is developed to solve the
problem of fault-tolerant control for a rigid spacecraft attitude stabilization manoeuvre in the …