Add to ORKGThere is an increasing demand for integrating unmanned aerial vehicles (UAVs) into civilian airspaces. Consequently, onboard systems should be evaluated for possible threats to human life. This paper discusses future certification requirements for flight control actuators. A scheme is proposed for evaluating reliability requirements for flight control electro-mechanical actuators (EMAs) considering different flight control configurations. This work is part of the TEMA-UAV project, which aims at developing certifiable fault-tolerant actuation for future UAVs
This book presents recent results on fault diagnosis and condition monitoring of airborne electromec...
The thesis aims to develop a Fault Tolerant Control (FTC) architecture, for the case of a damaged ac...
AbstractThis paper investigates safety requirements analysis of unmanned aero vehicle flight control...
There is an increasing demand for integrating unmanned aerial vehicles (UAVs) into civilian airspace...
There is an increasing demand for integrating unmanned aerial vehicles (UAVs) into civilian airspace...
Rising civilian applications that make use of unmanned aerial vehicles (UAVs) demand crucial precaut...
Electro-mechanical actuators (EMAs) are a primary actuation technology for unmannedaerial vehicles (...
This paper describes the activities carried out by Alenia Aermacchi and Pisa University for the deve...
The Fly‐by‐Wire technology enables flexible shaping of both effective dynamics and handling qualitie...
Unmanned Aerial Vehicles (UAVs) undergo fastgrowing integration into civilian airspace. Recently, th...
This chapter presents a selection of fault diagnosis problems related to airborne Electro-Mechanical...
International audienceFuture unmanned aerial vehicles (UAVs) will be designed toachieve their missio...
Abstract: A reliability assessment framework is presented for small unmanned aerial vehicles. The an...
This chapter presents the basic reliability and safety concerns related to the development of airbor...
The paper describes the initial results of a research activity aimed at developing a high integrity ...
This book presents recent results on fault diagnosis and condition monitoring of airborne electromec...
The thesis aims to develop a Fault Tolerant Control (FTC) architecture, for the case of a damaged ac...
AbstractThis paper investigates safety requirements analysis of unmanned aero vehicle flight control...
There is an increasing demand for integrating unmanned aerial vehicles (UAVs) into civilian airspace...
There is an increasing demand for integrating unmanned aerial vehicles (UAVs) into civilian airspace...
Rising civilian applications that make use of unmanned aerial vehicles (UAVs) demand crucial precaut...
Electro-mechanical actuators (EMAs) are a primary actuation technology for unmannedaerial vehicles (...
This paper describes the activities carried out by Alenia Aermacchi and Pisa University for the deve...
The Fly‐by‐Wire technology enables flexible shaping of both effective dynamics and handling qualitie...
Unmanned Aerial Vehicles (UAVs) undergo fastgrowing integration into civilian airspace. Recently, th...
This chapter presents a selection of fault diagnosis problems related to airborne Electro-Mechanical...
International audienceFuture unmanned aerial vehicles (UAVs) will be designed toachieve their missio...
Abstract: A reliability assessment framework is presented for small unmanned aerial vehicles. The an...
This chapter presents the basic reliability and safety concerns related to the development of airbor...
The paper describes the initial results of a research activity aimed at developing a high integrity ...
This book presents recent results on fault diagnosis and condition monitoring of airborne electromec...
The thesis aims to develop a Fault Tolerant Control (FTC) architecture, for the case of a damaged ac...
AbstractThis paper investigates safety requirements analysis of unmanned aero vehicle flight control...