This study proposes an uncertain optimal attitude–vibration control method for rigid–flexible
coupling satellites with reliability constraints based on the interval dimension-wise analysis …

Considering the multi-source uncertainties and disturbances in the attitude dynamics of
space power satellite (SPS), an interval dynamic model of SPS is proposed based on the …

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 considers the problems of control performance degradation caused by the
vibration of flexible accessories and external disturbance during the attitude maneuvering …

To realize high-precision attitude stabilization of a flexible spacecraft in the presence of
complex disturbances and measurement noises, an iterative learning disturbance observer …

This paper investigates the attitude control problem for flexible spacecraft subject to actuator
deadzone under event-trigger mechanism. An event-triggered mechanism is evolved to …

In this study, two distributed control strategies without or with a Partial Differential Equation
(PDE) observer are proposed for a team of flexible spacecraft to track the attitude of a virtual …

This work develops a novel multi-objective optimization for a robust attitude determination
method using the narrow bound theory, which is more appropriate to the limited uncertain …

H∞ control is well-known for its robustness performance, but the spacecraft attitude H∞
controller design under actuator misalignments and disturbances remains unexplored. In …

In this study, the integrated fault estimation (FE) and fault tolerant control (FTC) design
problem is investigated for the attitude system of a rigid spacecraft with inertia uncertainty …