Add to ORKGThis paper describes ongoing research to develop a framework for implementing dynamically reconfiguring avionics and control systems for unmanned aerial vehicles (UAVs) and a test and development environment for experimental UAVs. The framework supports graceful degradation, where hardware and software failures cause a reduction in the quality or capability of the control system but does not result in total system failure. The approach uses a graphical specification representing modular software interdependencies and a runtime system manager that reconfigures the system. The techniques are currently bein
In this paper we present a system for operation and testing of different UAVs. The system allows ea...
Following a brief description of the program involving the realization of a rotary wing uninhabited ...
In this paper, we address the problem of the reconfiguration of flight control systems after subsyst...
The goal of this research is to develop a framework for the design and implementation of reliable av...
With the recent advent of cost-effective and increasingly capable unmanned aerial vehicles (UAV), a ...
Ukraine Section SP/AES Joint ChapterThe paper shows how dynamic hardware-in-the-loop ground test s...
In applications involving unmanned aerial vehicles, the use of simulation environments is typically ...
One of the important steps in Flight Management Systems (FMS) development is its testing in the dyna...
A simulation environment is developed at West Virginia University to support the design and testing ...
The aim of the paper is to present a dynamic control allocation architecture for the design and deve...
This paper presents a Matlab/Simulink simulation environment developed at West Virginia University t...
This paper presents a non linear automatic UAV simulation testbed and an autonomous control implemen...
Unmanned air systems are becoming increasingly pervasive in academia as well as industry. Aerospace ...
In the paper, influence of control surface failures on UAV aircraft dynamics is investigated. A meth...
The paper considers the experience of the manned aircraft modification to UAVs and technological sol...
In this paper we present a system for operation and testing of different UAVs. The system allows ea...
Following a brief description of the program involving the realization of a rotary wing uninhabited ...
In this paper, we address the problem of the reconfiguration of flight control systems after subsyst...
The goal of this research is to develop a framework for the design and implementation of reliable av...
With the recent advent of cost-effective and increasingly capable unmanned aerial vehicles (UAV), a ...
Ukraine Section SP/AES Joint ChapterThe paper shows how dynamic hardware-in-the-loop ground test s...
In applications involving unmanned aerial vehicles, the use of simulation environments is typically ...
One of the important steps in Flight Management Systems (FMS) development is its testing in the dyna...
A simulation environment is developed at West Virginia University to support the design and testing ...
The aim of the paper is to present a dynamic control allocation architecture for the design and deve...
This paper presents a Matlab/Simulink simulation environment developed at West Virginia University t...
This paper presents a non linear automatic UAV simulation testbed and an autonomous control implemen...
Unmanned air systems are becoming increasingly pervasive in academia as well as industry. Aerospace ...
In the paper, influence of control surface failures on UAV aircraft dynamics is investigated. A meth...
The paper considers the experience of the manned aircraft modification to UAVs and technological sol...
In this paper we present a system for operation and testing of different UAVs. The system allows ea...
Following a brief description of the program involving the realization of a rotary wing uninhabited ...
In this paper, we address the problem of the reconfiguration of flight control systems after subsyst...