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 study surveys the developments in satellite attitude determination and control system,
especially for microsats. This survey is not intended to be complete but is limited to the most …

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 …

In this paper, a fast terminal sliding mode control (FTSMC) scheme with double closed loops
is proposed for the spacecraft attitude control. The FTSMC laws are included both in an …

This paper is devoted to the attitude and vibration control of spacecraft containing flexible
appendages. It entails an investigation of a passive control strategy which consists in …

In this article, anti-unwinding attitude maneuver control for rigid spacecraft is considered.
First, in order to avoid the unwinding phenomenon when the system states are restricted to …

Variable stiffness vibration isolator (VSVI) can be switched between the low stiffness state
and high stiffness state, respectively suitable for spacecraft requirement in cutting off the jitter …

In this article, active vibration suppression and attitude control for flexible spacecraft under
model uncertainty and external disturbance are investigated. First, an adaptive disturbance …

Attitude control and power storage subsystems are two of the essential utilities provided on a
spacecraft. As they comprise a significant fraction of a spacecraft mass, a synergism concept …

In this paper the three axes slewing maneuver and the vibration suppression of a flexible
spacecraft are studied. The satellite has a central rigid body and two flexible appendages …