The science objectives of a spacecraft mission place stringent performance requirements on
the spacecraft attitude control system. However, it remains an open problem how to …

A novel fault tolerant attitude tracking control scheme is developed for flexible spacecraft
with partial loss of actuator effectiveness fault. Neural networks are first introduced to …

A novel finite-time controller integrated with disturbance observer is investigated for a rigid
spacecraft in the presence of disturbance, actuator saturation and misalignment. As a …

This paper investigates the velocity-measurement-free feedback control problem associated
with attitude tracking for a rigid spacecraft in the presence of both actuator failures and …

In this paper, a fault-tolerant control scheme is proposed for the rigid spacecraft attitude
control system subject to external disturbances, multiple system uncertainties, and actuator …

A method requiring low-computational overhead is presented which generates low-torque
reference motions between arbitrary orientations for a spin-stabilized spacecraft. The initial …

In this paper, we propose new robust optimal control strategies for spacecraft position and
attitude tracking maneuvers in the presence of external disturbances. First, two optimal …

This paper investigates the problem of finite-time output feedback control for spacecraft
attitude stabilization with attitude-only measurement. First, a finite-time filter is proposed to …

This paper addresses the problem of robust optimal control of spacecraft attitude
stabilization in the presence of parametric uncertainties, external disturbances and actuator …

Spacecraft Attitude Control: A Linear Matrix Inequality Approach solves problemsfor
spacecraft attitude control systems using convex optimization and, specifi cally, through a …