Redirigiendo al acceso original de articulo en 16 segundos...
Inicio  /  Applied Sciences  /  Vol: 12 Par: 13 (2022)  /  Artículo
ARTÍCULO
TITULO

Multirotor Unmanned Aerial Vehicle Configuration Optimization Approach for Development of Actuator Fault-Tolerant Structure

Yisak Debele    
Ha-Young Shi    
Assefinew Wondosen    
Jin-Hee Kim and Beom-Soo Kang    

Resumen

The proposed approach can be utilized to support the design of novel actuator fault-tolerant multirotor configurations capable of performing desired maneuvers.

 Artículos similares

       
 
Petar Piljek, Denis Kotarski and Matija Krznar    
Due to their abilities, multirotor unmanned aerial vehicles (UAVs) can be used in various missions that require complex and precise movements, so they are a typical representative of aerial robots. Since this type of UAV is characterized by high energy c... ver más
Revista: Applied Sciences

 
Przemyslaw Tymków, Grzegorz Józków, Agata Walicka, Mateusz Karpina and Andrzej Borkowski    
The paper presents an efficient methodology of water body extent estimation based on remotely sensed data collected with UAV (Unmanned Aerial Vehicle). The methodology includes the data collection with selected sensors and processing of remotely sensed d... ver más
Revista: Water

 
Cengiz Koparan, Ali Bulent Koc, Charles V. Privette, Calvin B. Sawyer and Julia L. Sharp    
Water quality assessment programs for the management of water resources require the collection of water samples for physical, chemical, and biological analyses. Lack of personnel, accessibility of water bodies, and time constraints, especially after natu... ver más
Revista: Water

 
Hriday Bavle, Jose Luis Sanchez-Lopez, Paloma de la Puente, Alejandro Rodriguez-Ramos, Carlos Sampedro and Pascual Campoy    
This paper presents a fast and robust approach for estimating the flight altitude of multirotor Unmanned Aerial Vehicles (UAVs) using 3D point cloud sensors in cluttered, unstructured, and dynamic indoor environments. The objective is to present a flight... ver más
Revista: Aerospace

 
Mantas Brazinskas, Stephen D. Prior and James P. Scanlan    
The majority of research into full-sized helicopter overlapping propulsion systems involves co-axial setups (fully overlapped). Partially overlapping rotor setups (tandem, multirotor) have received less attention, and empirical data produced over the yea... ver más
Revista: Aerospace