Given the few unsuccessful space missions in the past few decades, designing a fault-
tolerant spacecraft's attitude control has piqued the scientific and academic community's …

Reliable spacecraft's attitude control is one of the core research areas of the space industry
due to the need for sustainable space exploration and advancements in space technology …

In this paper, a finite-time active fault-tolerant control scheme is designed for a flexible
spacecraft's attitude control experiencing inertial parametric variations, external …

This paper studies the attitude tracking problem for rigid spacecraft under restricted
communication resources. This work proposes a novel composite control scheme for …

This article considers the problem of attitude regulation of rigid spacecraft under the effect of
inertial ambiguity, exogenous disturbances, input saturation, and actuator uncertainties. In …

This paper investigates the attitude controller design for the reusable launch vehicle (RLV)
in its re-entry phase under the influence of model uncertainties and external disturbances …

AT–S fuzzy-based sliding mode observer (SMO)-based fault detection scheme is conducted
to realize the actuator fault detection issue, including stuck fault detection and partial loss of …

This article investigates the application of hysteresis quantizer for the spacecraft regulation
problem under a constrained network. The hysteresis quantizer helps in quantizing the …

In this paper, a data-driven optimal time-delayed control (TDC) approach is developed for
Euler–Lagrange systems and applied to an aerial manipulator. The proposed approach is …

In this paper, the rigid spacecraft rendezvous problem is studied in the sense of fully-
actuated system. According to the attitude and orbit dynamics, the fully-actuated system …