Add to ORKGThe NASA AirSTAR system has been designed to address the challenges associated with safe and efficient subscale flight testing of research control laws in adverse flight conditions. In this paper, software elements of this system are described, with an emphasis on components which allow for rapid prototyping and deployment of aircraft control laws. Through model-based design and automatic coding a common code-base is used for desktop analysis, piloted simulation and real-time flight control. The flight control system provides the ability to rapidly integrate and test multiple research control laws and to emulate component or sensor failures. Integrated integrity monitoring systems provide aircraft structural load protection, isolate the sys...
Due to the character of the original source materials and the nature of batch digitization, quality ...
The usage of light utility high aspect ratio aircraft with payload up to 350kg is deemed to be an ec...
This paper presents a historical overview of research in reconfigurable flight control with a focus ...
Avionics, like any other safety-critical real-time systems, pose unique challenges on system design,...
The primary objective of this thesis was to study, implement, and test low-cost electronic flight co...
Safety and reliability are key if unmanned aerial systems (UAS) are to move from research and become...
Flight control system software is a critical component of the digital flight control computer of lig...
The Aerospace Engineering of the TU Delft operates a Cessna Citation II laboratory aircraft. The air...
To maintain nominal flight control system functionalities during fault scenarios, enhancements of th...
Fly-by-wire systems are becoming increasingly common in civil transport aircraft due to the economic...
Two major safety-critical elements of the onboard software for the Tejas digital flight controlcompu...
The Delft University laboratory aircraft Cessna Citation II has the capability to implement and test...
These slides discuss the flight software testing methodology and examples of applying these methods ...
Following a brief description of the program involving the realization of a rotary wing uninhabited ...
The design, implementation, and verification of the flight control software used in the F-8 DFBW pro...
Due to the character of the original source materials and the nature of batch digitization, quality ...
The usage of light utility high aspect ratio aircraft with payload up to 350kg is deemed to be an ec...
This paper presents a historical overview of research in reconfigurable flight control with a focus ...
Avionics, like any other safety-critical real-time systems, pose unique challenges on system design,...
The primary objective of this thesis was to study, implement, and test low-cost electronic flight co...
Safety and reliability are key if unmanned aerial systems (UAS) are to move from research and become...
Flight control system software is a critical component of the digital flight control computer of lig...
The Aerospace Engineering of the TU Delft operates a Cessna Citation II laboratory aircraft. The air...
To maintain nominal flight control system functionalities during fault scenarios, enhancements of th...
Fly-by-wire systems are becoming increasingly common in civil transport aircraft due to the economic...
Two major safety-critical elements of the onboard software for the Tejas digital flight controlcompu...
The Delft University laboratory aircraft Cessna Citation II has the capability to implement and test...
These slides discuss the flight software testing methodology and examples of applying these methods ...
Following a brief description of the program involving the realization of a rotary wing uninhabited ...
The design, implementation, and verification of the flight control software used in the F-8 DFBW pro...
Due to the character of the original source materials and the nature of batch digitization, quality ...
The usage of light utility high aspect ratio aircraft with payload up to 350kg is deemed to be an ec...
This paper presents a historical overview of research in reconfigurable flight control with a focus ...