Add to ORKGThis project consists of the design and development of a navigational unit for a UAV (Unmanned Air Vehicle). The purpose is to design from scratch a device that would use three accelerometers, three gyroscopes, a magnetometer and a GPS to provide an estimation of the angular position of the UAV. The tasks involved selecting appropriate sensors, designing a circuit board, assembling the board, connecting the sensors and testing them. A mathematical model of the plane dynamics was also provided to increase the accuracy of the measurement. One extra task was to translate this model, provided in MatLab, into C code.Validerat; 20101217 (root
Changing the position of the Center of Gravity (CoG) for an aerial vehicle is a challenging part in...
This paper presents the development of a low cost miniature navigation system for autonomous flying ...
This paper presents an innovative integrated navigation unit developed for small unmanned aircraft s...
This project consists of the design and development of a navigational unit for a UAV (Unmanned Air...
In the CDIO-project course in Automatic Control, an Autonomous Unmanned Aerial vehicle (UAV) is cons...
This paper describes a modeling and designing of inertial sensor using Inertial Measurement Unit (IM...
Because of the limitation of GPS indoors there is a demand for alternative methods to accurately det...
The authors present the results of numerical experiments aimed to determine the mean square error, w...
As world manufacturing technologies nowadays are transforming to industry revolution 4.0, autonomous...
The use of Unmanned Aerial Vehicles (UAVs) has rapidly increased over the last years. This has been ...
In many unmanned aerial vehicle (UAV) applications a direct georeferencing is required. The reason c...
For the safe operation of Unmanned Aerial Vehicles (UAVs), an effective Automatic Control System (ACS...
International audienceThis paper deals with the design, construction, and instrumentation of a UAV e...
This paper discusses the development of a low-cost, redundant, strapdown inertial measurement unit (...
This paper presents a new design and development of a low cost GPS (Global Positioning System)-aided...
Changing the position of the Center of Gravity (CoG) for an aerial vehicle is a challenging part in...
This paper presents the development of a low cost miniature navigation system for autonomous flying ...
This paper presents an innovative integrated navigation unit developed for small unmanned aircraft s...
This project consists of the design and development of a navigational unit for a UAV (Unmanned Air...
In the CDIO-project course in Automatic Control, an Autonomous Unmanned Aerial vehicle (UAV) is cons...
This paper describes a modeling and designing of inertial sensor using Inertial Measurement Unit (IM...
Because of the limitation of GPS indoors there is a demand for alternative methods to accurately det...
The authors present the results of numerical experiments aimed to determine the mean square error, w...
As world manufacturing technologies nowadays are transforming to industry revolution 4.0, autonomous...
The use of Unmanned Aerial Vehicles (UAVs) has rapidly increased over the last years. This has been ...
In many unmanned aerial vehicle (UAV) applications a direct georeferencing is required. The reason c...
For the safe operation of Unmanned Aerial Vehicles (UAVs), an effective Automatic Control System (ACS...
International audienceThis paper deals with the design, construction, and instrumentation of a UAV e...
This paper discusses the development of a low-cost, redundant, strapdown inertial measurement unit (...
This paper presents a new design and development of a low cost GPS (Global Positioning System)-aided...
Changing the position of the Center of Gravity (CoG) for an aerial vehicle is a challenging part in...
This paper presents the development of a low cost miniature navigation system for autonomous flying ...
This paper presents an innovative integrated navigation unit developed for small unmanned aircraft s...