Zobrazeno 1 - 10
of 32
pro vyhledávání: '"Carlos Perez-Montenegro"'
Publikováno v:
Producción + Limpia. 13:7-18
Introduccion. La comunidad, entendida como grupo social a diferentes escalas como hogar, barrio, pueblo, industria, ciudad, tiene la responsabilidad de los cambios en el entorno en que vive; estas transformaciones tienen su origen en las decisiones q
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::0175b9c59340ddd22efea605ac7d2fd5
https://doi.org/10.22507/pml.v13n1a1
https://doi.org/10.22507/pml.v13n1a1
Autor:
Nicoletta Bloise, Matteo Scanavino, Giorgio Guglieri, Carlos Perez-Montenegro, Elisa Capello, Alessandro Rizzo
Publikováno v:
Transportation Research Procedia. 35:110-119
The use of Unmanned Aerial Vehicles (UAVs) is now common, but although they have been for various applications, there are still a lot of challenges that need to be overcome. One key issue is related to standardizing the use of these vehicles in urban
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::39c9692192c1b785c6e54f3631203e41
https://doi.org/10.1016/j.trpro.2018.12.018
https://doi.org/10.1016/j.trpro.2018.12.018
Publikováno v:
ECC
Unmanned Aerial Vehicles (UAVs) have been successfully employed in cooperative tasks over recent years, particularly in the applications for smart cities. In such scenario, a networked control system (NCS) framework is usually adopted since measureme
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::55fd817de9a2902d8983e7ace704aeae
https://doi.org/10.23919/ecc.2019.8796087
https://doi.org/10.23919/ecc.2019.8796087
Autor:
Carlo Novara, Enrico Canuto, Carlos Perez-Montenegro, Mauricio Alejandro Lotufo, Luigi Colangelo
This study presents an original approach to the design of a complete digital attitude control unit for a UAV quadrotor. The approach is developed within the framework of Active Disturbance Rejection Control (ADRC) and Embedded Model Control (EMC), tw
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::08b2bb6d7ab2e575a138ec6e57d49fe4
http://hdl.handle.net/11583/2719171
http://hdl.handle.net/11583/2719171
This chapter is concerned with force and torque actuators. Force actuators may be used by orbit and attitude control systems. To generate a torque, the force vector must not pass through the spacecraft center of mass. Typical force actuators are mass
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::383a2d3397b669f67146b14aceea4fbd
https://doi.org/10.1016/b978-0-08-100700-6.00009-x
https://doi.org/10.1016/b978-0-08-100700-6.00009-x
Publikováno v:
Spacecraft Dynamics and Control
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::804899e1177efa84bc2094de881895b5
https://doi.org/10.1016/b978-0-08-100700-6.00005-2
https://doi.org/10.1016/b978-0-08-100700-6.00005-2
This chapter is concerned with spacecraft sensors as part of position and attitude control loops. It will discuss the principal sensors for the determination of on-board orientation and orbit position. The working principles of these sensors are outl
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::236df28f2fd3944df6a247a4e946680e
https://doi.org/10.1016/b978-0-08-100700-6.00008-8
https://doi.org/10.1016/b978-0-08-100700-6.00008-8