A generic software error in the quadruply redundant primary flight system could result in the catastrophic loss of Space Shuttle vehicle control in the hostile environment of ascent or reentry. The Space Shuttle backup flight system was designed to protect the crew and vehicle In this eventuality. The significant challenges met in the design and development of this state-of-the-art protective system Is the subject of thls paper
Concepts for software to implement real time aircraft control systems on a centralized digital compu...
Abstract: System redundancy in aircraft is very important as it ensures faulty components would not ...
The development of fault tolerant embedded control systems, such as flight control systems (FCS) are...
Modern technological and safety‐critical systems rely on sophisticated control solutions to meet inc...
The development and verification of the Backup Flight System software (BFS) is discussed. The approa...
The challenge of providing redundancy management (RM) and fault tolerance to meet the Shuttle Progra...
A number of inventors and entrepreneurs are currently attempting to develop and commercially operate...
To maintain nominal flight control system functionalities during fault scenarios, enhancements of th...
The article presents suggestions on the synthesis of tolerant digital systems of management flight b...
A new fault-tolerant system software concept employing the primary digital computers as host for the...
Software plays an increasingly larger role in all aspects of NASA's science missions. This has been ...
Surveying the current state of practice of spacecraft autonomy, one can detect many different attrib...
The reliability of electronic systems is a significant challenge in the development of new devices.I...
Modern technological and safety-critical systems rely on sophisticated control solutions to meet inc...
This research addresses the high CubeSat mission failure rates caused by inadequate software and ove...
Concepts for software to implement real time aircraft control systems on a centralized digital compu...
Abstract: System redundancy in aircraft is very important as it ensures faulty components would not ...
The development of fault tolerant embedded control systems, such as flight control systems (FCS) are...
Modern technological and safety‐critical systems rely on sophisticated control solutions to meet inc...
The development and verification of the Backup Flight System software (BFS) is discussed. The approa...
The challenge of providing redundancy management (RM) and fault tolerance to meet the Shuttle Progra...
A number of inventors and entrepreneurs are currently attempting to develop and commercially operate...
To maintain nominal flight control system functionalities during fault scenarios, enhancements of th...
The article presents suggestions on the synthesis of tolerant digital systems of management flight b...
A new fault-tolerant system software concept employing the primary digital computers as host for the...
Software plays an increasingly larger role in all aspects of NASA's science missions. This has been ...
Surveying the current state of practice of spacecraft autonomy, one can detect many different attrib...
The reliability of electronic systems is a significant challenge in the development of new devices.I...
Modern technological and safety-critical systems rely on sophisticated control solutions to meet inc...
This research addresses the high CubeSat mission failure rates caused by inadequate software and ove...
Concepts for software to implement real time aircraft control systems on a centralized digital compu...
Abstract: System redundancy in aircraft is very important as it ensures faulty components would not ...
The development of fault tolerant embedded control systems, such as flight control systems (FCS) are...