This paper proposes a novel neural adaptive fixed-time control approach for the attitude
stabilization and vibration suppression of flexible spacecraft. First, the neural network (NN) …

This paper presents a robust fuzzy tracking controller for position and attitude control, and for
vibration suppression in a flexible spacecraft. The robust fuzzy controller guarantees H∞ …

This paper presents and compares two fuzzy controllers for attitude stabilization of a
spacecraft with partially filled fuel tank: a fuzzy controller based on the parallel distributed …

This paper investigates the performance of a fuzzy optimal variance control technique for
attitude stability and vibration attenuation with regard to a spacecraft made of a rigid platform …

In this paper, a dynamics equation for Spacecraft has first been created using vector
mechanics. Second, several attitude dynamics equations of spacecraft have been deduced …

Attitude stabilization control via disturbance observer for flexible spacecraft is studied in this
paper. First, a model based on Takagi-Sugeno fuzzy system of flexible spacecraft is …

This paper develops an intelligent attitude control and vibration suppression system for
flexible spacecraft performing a single-axis maneuver with external disturbances and …

This paper investigates the performance of a fuzzy optimal variance control technique for
attitude stability and vibration attenuation with regard to a spacecraft made of a rigid platform …

During the upper-stage separation and orbit injection, orbital control, and attitude maneuver,
propellant slosh in partially-filled fuel tanks can cause dynamical instability or pointing …