In this work, the optimization by genetic algorithms of a system based on fuzzy logic for the attitude control of a nanosatellite is performed. The objective of this optimization is to propose different designs of the fuzzy controller depending on the possible operation modes along the whole mission of the satellite, to improve its efficiency and performance.
The Discrete EVent System Specification (DEVS) formalism provides a unified method to define any discrete-event system accurately. As the complexity of the system under study increases, the necessity of simulation engines with higher performance rises.
Modeling, Simulation, and Optimization tools are used in the development process of complex systems for improving their overall performance. However, enforcing full coverage in the…
The appearance of two-phase immersion cooling systems enables the deployment of small, low-consumption edge data centers. However, the characterization of dielectric coolants requires a monitoring,…
The demand of novel IoT and smart city applications is increasing significantly and it is expected that by 2020 the number of connected devices will…
The technological revolution of the Internet of Things (IoT) is transforming our society by registering and analyzing users and infrastructures’ behavior in order to develop…