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∞ …

Previous studies have shown that the absolute coordinate-based formulation is an accurate
modeling approach for the rigid-flexible multibody system subject to both large rotation and …

This paper studies the station-keeping control of underactuated stratospheric airships in the
presence of model uncertainties and wind field, and a T–S fuzzy model-based adaptive …

TO CONTROL launch costs, materials with low density are extensively used in the design of
spacecraft appendages, such as solar panels, flexible antennas, and robot manipulators …

At present, rigid-flexible coupling systems have been used in various engineering fields
extensively, due to task demands, the systems have become complex increasingly, and …

In this paper, the attitude stabilization of flexible spacecraft with unmeasurable states and
disturbances is addressed by an observer-based fuzzy integral sliding mode control …

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 …

This paper presents a robust-optimal fuzzy controller for position and attitude stabilization
and vibration suppression of a flexible spacecraft during antenna retargeting maneuver. The …

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 …

This paper presents a robust-optimal fuzzy controller for position and attitude stabilization,
and vibration suppression of a flexible spacecraft during antenna retargeting maneuver. The …