This article presents the development of an anti-windup (AW) compensator architecture for
nanosatellite systems. The design addresses the problem of fault-tolerant control (FTC) for …

Here we present the development and qualification of the highly integrated satellite avionics
stack of ESTCube-2, a three-unit CubeSat carrying various in-orbit demonstration payloads …

The development of attitude control systems in recent years have increasingly focused on
Fault Tolerant Control (FTC) capabilities to deal with sensor and actuator faults as well as …

This research explores the application and performance of the Linear Quadratic Regulator
(LQR) and Model Predictive Controller (MPC) in satellite attitude control. The study involves …

Attitude control for small satellites is recently given particular concern. This paper has
designed Proportional Derivative and Linear Quadratic Regulator controllers. A comparative …

Mathematical modeling of attitude control system for a nano-satellite has been developed
based on reaction wheels as a primary actuator. Environmental disturbing torques have …

This study investigates the application of an optimal control algorithm to solve a satellite
attitude control problem. The study entails obtaining the satellite equations of motion through …

This paper presents the design of attitude control systems for autonomous spacecraft subject
to noisy measurements from sensors, external, and internal disturbances. The objective is to …

In this article, a new approach has been presented in the design of a satellite attitude
controller using reaction wheels. First, a PID control structure whose coefficients are …

Este documento es un informe para optar por el título de licenciado en ingeniería en
mecatrónica. En este se presenta la metodología para el diseño de un controlador clásico y …