Motivated by several accidents, attitude control of a spacecraft subject to faults/failures has
gained considerable attention in a wider range of aerospace engineering and academic …

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 …

In this paper we address control systems with redundant actuators and characterize the
concepts of weak and strong input redundancy. Based on this characterization, we propose …

This Review discusses the main results obtained in training end-to-end neural architectures
for guidance and control of interplanetary transfers, planetary landings, and close-proximity …

In this study, the authors propose two non-linear attitude controllers, mainly consisting of the
sliding-mode attitude tracking controller and the sliding-mode adaptive attitude tracking …

Inspired by the integrated guidance and control design for endo-atmospheric aircraft, the
integrated position and attitude control of spacecraft has attracted increasing attention and …

In this paper, a constrained control allocation scheme is designed based on the
neurodynamic model for an overactuated aircraft with system uncertainties and unknown …

Satellites clusters for Earth observation purposes entail precise orbit monitoring and control
to satisfy application needs efficiently. Fast technological progress in GNSS receivers …

Use of actuator redundancy to achieve higher reliability is a widely accepted engineering
design technique and is used in this study to build resiliency and ensure power system …

A methodology for the design of two-layer hierarchical control systems is presented. The
high layer corresponds to a system with slow dynamics, whose control inputs must be …