A high-order fully actuated (HOFA) system approach is proposed for the attitude control
problem of a flexible spacecraft with nonlinear and time-varying inertia. Different from most …

This paper introduces an Optimal Fuzzy Sliding Mode (OFSM) controller for the control of
fuel sloshing in a spacecraft during orbital maneuvers. In order to optimize controller's gains …

In the present study, a predefined-time attitude stabilization for liquid-filled spacecraft with
large liquid sloshing is investigated under input saturation and external disturbance. First …

In this article, optimum adaptive sliding mode controller (ASMC) optimized by particle swarm
optimization (PSO) algorithm is designed to solve the trajectory tracking control problems of …

In this paper, a comparison between optimal adaptive and fuzzy control methods is
performed for the problem of satellite attitude control. The optimal adaptive controller is …

Due to significance of high-accuracy attitude control, the fuel sloshing effects on the satellite
attitude should be considered, more precisely. This work deals with the attitude control of a …

Quadrotors suspended water containers may be used for fire-fighting services.
Unfortunately, the complicated dynamics in this type of system degrade the flight safety …

This paper introduces a flexible framework to enable high-fidelity simulations of the fuel
slosh dynamics for verification of the Guidance, Navigation and Control (GNC) algorithms …

In the attitude tracking control tasks of rigid bodies with partially filled cavities, liquid sloshing
is a crucial characteristic that hinders effective controller design and accuracy improvement …

This paper is concerned with the attitude tracking control problem of liquid-filled spacecraft
with large liquid sloshing. In existing work, the force and torque generated by liquid sloshing …