A robust fixed-time control framework is presented to stabilize flexible spacecraft's attitude
system with external disturbance, uncertain parameters of inertia, and actuator uncertainty …

This paper investigates the attitude tracking problem for the flexible spacecraft composed of
a rigid platform with a rotating appendage. Two robust attitude controllers, each matched to …

An efficient and cost-effective finite-time fault-tolerant attitude controller for a class of flexible
spacecraft is designed in this paper to cater to flexible appendages' vibrations, along with …

Abstract A Generalized Differential Quadrature (GDQ) as an accurate numerical technique
based on non-uniform grid point distribution, Chebyshev-Gauss-Lobatto (CGL) and Roots of …

In this paper, the dynamic modeling of a new configuration spacecraft is investigated. The
significance of dumbbell-shaped spacecraft to deep space exploration and the configuration …

A modified neural network-based disturbance observer with high-accuracy estimation
performance is fabricated for spacecraft attitude control in this paper. To reduce the …

One of the major needs of future Earth Observation satellites is to fulfil high demanding
pointing requirements when using instrumentations supported by or mounted at the end of …

The vibration of flexible solar array during sun-tracking drive has been one of the
challenging problems in modern space technology. In this work, the vibration disturbance of …

High precision attitude stabilization of spacecraft is essential for the operation of precision
instruments onboard. However, attitude vibrations of spacecraft are inevitably induced by …

In this paper, control moment gyroscope (CMG) system is employed to suppress vibration of
flexible spacecraft during attitude maneuver. Direct modal force generated by CMGs is …