International audienceThe failure of hardware or software in a critical system can lead to loss of lives. Design errors are a major source of the defects that can be introduced during the system devel- opment. A complementary approach like formal methods is considered as an alternative approach to identify the possible defects in the software development process using rigorous mathematical reasoning. The increasing system complexity and failure rate invoke the area of verification and validation of avionic systems. This paper describes a stepwise formal development of an aircraft landing system using Event-B. The formal models include the complex behaviour, tempo- ral behaviour and sequence of operations of a landing gear system. The refine...
International audienceWe describe our experience with modeling the landing gear system of an aircraf...
International audienceIn this case study we test a landing gear control system of a military aircraf...
This report is based on one prepared as a chapter for the FAA Digital Systems Validation Handbook (a...
International audienceThe failure of hardware or software in a critical system can lead to loss of l...
The failure of hardware or software in a critical system can lead to loss of lives. The design error...
International audienceThis paper presents a step wise formal development oft helanding system of an ...
The size and complexity of control software in aerospace systems is rapidly increasing, and this de...
Embedded critical systems need to be validated very thoroughly; it usually results in very long and ...
When designing and developing systems in safety critical or cost intensive environments it is import...
A verification case study of a complex real-time system from the automotive area, an emergency brake...
We describe our experience with modeling the landing gear system of an aircraft using the formal spe...
Today, large civil aircraft incorporate a vast array of complex and coupled subsystems with thousand...
This document summarizes the safety analysis performed on a Flight Guidance System (FGS) requirement...
We analyze the functionality of the landing system of a regional aircraft in the extension and cruis...
Symbolic algebraic analysis techniques are applied to the landing gear subsystem in the Swedish figh...
International audienceWe describe our experience with modeling the landing gear system of an aircraf...
International audienceIn this case study we test a landing gear control system of a military aircraf...
This report is based on one prepared as a chapter for the FAA Digital Systems Validation Handbook (a...
International audienceThe failure of hardware or software in a critical system can lead to loss of l...
The failure of hardware or software in a critical system can lead to loss of lives. The design error...
International audienceThis paper presents a step wise formal development oft helanding system of an ...
The size and complexity of control software in aerospace systems is rapidly increasing, and this de...
Embedded critical systems need to be validated very thoroughly; it usually results in very long and ...
When designing and developing systems in safety critical or cost intensive environments it is import...
A verification case study of a complex real-time system from the automotive area, an emergency brake...
We describe our experience with modeling the landing gear system of an aircraft using the formal spe...
Today, large civil aircraft incorporate a vast array of complex and coupled subsystems with thousand...
This document summarizes the safety analysis performed on a Flight Guidance System (FGS) requirement...
We analyze the functionality of the landing system of a regional aircraft in the extension and cruis...
Symbolic algebraic analysis techniques are applied to the landing gear subsystem in the Swedish figh...
International audienceWe describe our experience with modeling the landing gear system of an aircraf...
International audienceIn this case study we test a landing gear control system of a military aircraf...
This report is based on one prepared as a chapter for the FAA Digital Systems Validation Handbook (a...