The paper presents an integrated inertial measurement unit based on an innovative redundant configuration of low-cost Micro-Electro-Mechanical Sensors for small unmanned aircraft systems. The prototype developed consists of six different IMU in a cubic configuration with triaxial gyroscopes, accelerometers, and magnetometers. The redundancy allows improving the performance of the system because of the mutual calibration of single sensors. The performance of the prototype are preliminarily assess through short flight sessions. The attitude measures obtained from multiple-IMU turns out to be compliant with requirements for drone navigation
In this paper a Fault Tolerant system for the attitude estimation of an Unmanned Aerial Vehicle (UAV...
In this paper a Fault Tolerant system for the attitude estimation of an Unmanned Aerial Vehicle (UAV...
In this paper a Fault Tolerant system for the attitude estimation of an Unmanned Aerial Vehicle (UAV...
The paper presents an integrated inertial measurement unit based on an innovative redundant configur...
This paper presents an innovative integrated navigation unit developed for small unmanned aircraft s...
This paper proposes an attitude determination system for small Unmanned Aerial Vehicles (UAV) with a...
This paper proposes an attitude determination system for small Unmanned Aerial Vehicles (UAV) with a...
This paper proposes an attitude determination system for small Unmanned Aerial Vehicles (UAV) with a...
This paper proposes an attitude determination system for small Unmanned Aerial Vehicles (UAV) with a...
We introduce a three step procedure to improve attitude determination by MEMS-IMU sensors on board a...
Inertial measurement units (IMUs) are fundamental for attitude control of drones. With the advanceme...
Inertial sensors and inertial measurement units (IMUs) are widely used in navigation support systems...
The paper presents an innovative strategy to measure the initial heading of a vehicle in the local r...
The paper presents an innovative strategy to measure the initial heading of a vehicle in the local r...
In this paper a Fault Tolerant system for the attitude estimation of an Unmanned Aerial Vehicle (UAV...
In this paper a Fault Tolerant system for the attitude estimation of an Unmanned Aerial Vehicle (UAV...
In this paper a Fault Tolerant system for the attitude estimation of an Unmanned Aerial Vehicle (UAV...
In this paper a Fault Tolerant system for the attitude estimation of an Unmanned Aerial Vehicle (UAV...
The paper presents an integrated inertial measurement unit based on an innovative redundant configur...
This paper presents an innovative integrated navigation unit developed for small unmanned aircraft s...
This paper proposes an attitude determination system for small Unmanned Aerial Vehicles (UAV) with a...
This paper proposes an attitude determination system for small Unmanned Aerial Vehicles (UAV) with a...
This paper proposes an attitude determination system for small Unmanned Aerial Vehicles (UAV) with a...
This paper proposes an attitude determination system for small Unmanned Aerial Vehicles (UAV) with a...
We introduce a three step procedure to improve attitude determination by MEMS-IMU sensors on board a...
Inertial measurement units (IMUs) are fundamental for attitude control of drones. With the advanceme...
Inertial sensors and inertial measurement units (IMUs) are widely used in navigation support systems...
The paper presents an innovative strategy to measure the initial heading of a vehicle in the local r...
The paper presents an innovative strategy to measure the initial heading of a vehicle in the local r...
In this paper a Fault Tolerant system for the attitude estimation of an Unmanned Aerial Vehicle (UAV...
In this paper a Fault Tolerant system for the attitude estimation of an Unmanned Aerial Vehicle (UAV...
In this paper a Fault Tolerant system for the attitude estimation of an Unmanned Aerial Vehicle (UAV...
In this paper a Fault Tolerant system for the attitude estimation of an Unmanned Aerial Vehicle (UAV...