The objective of the European research project SUPRA (Simulation of Upset Recovery in Aviation) is to develop technologies that eventually contribute to a reduction of risk of Loss of control - in flight (LOC-I) accidents, today's major cause of fatal accidents in commercial aviation. To this end the project developed novel concepts to improve groundbased simulation of upset events. Current flight simulators are considered inadequate for the simulation of many upset conditions as the flight dynamics and aerodynamic models apply only to the normal flight regimes and aircraft behavior may change significantly outside this envelope. Furthermore, standard hexapodbased motion systems are unable to reproduce the high accelerations, angular rates,...
The aim of the collaborative European research project ‘Simulation of UPset Recovery in Aviation’ (S...
Loss-of-control resulting from airplane upset is a leading cause of worldwide commercial aircraft ac...
The aerodynamic model of a generic airliner configuration is developed for a wide range of angles of...
The objective of the European research project SUPRA (Simulation of Upset Recovery in Aviation) is t...
The SUPRA research project - Simulation of Upset Recovery in Aviation - has been funded by the Europ...
The SUPRA research project – Simulation of Upset Recovery in Aviation – has been funded by the Europ...
The SUPRA research project - Simulation of Upset Recovery in Aviation - has been funded by the Europ...
The SUPRA research project – Simulation of Upset Recovery in Aviation – has been funded by the Europ...
The European research project SUPRA (“Simulation of Upset Recovery in Aviation”) produced an extende...
The collaborative research project SUPRA, intends to develop methodologies and advanced flight simul...
The paper presents the aerodynamic model in extended flight envelope for a generic airliner with und...
One of the primary objectives of the European Union 7th Framework Program research project SUPRA – “...
Aircraft departing from the nominal flight envelop and entering upset situations have become a major...
Currently, it is uncertain how well a typical ground-based simulator's hexapod motion system can sim...
Unsuccessful recovery from unusual flight attitudes, or airplane upset, is considered an important f...
The aim of the collaborative European research project ‘Simulation of UPset Recovery in Aviation’ (S...
Loss-of-control resulting from airplane upset is a leading cause of worldwide commercial aircraft ac...
The aerodynamic model of a generic airliner configuration is developed for a wide range of angles of...
The objective of the European research project SUPRA (Simulation of Upset Recovery in Aviation) is t...
The SUPRA research project - Simulation of Upset Recovery in Aviation - has been funded by the Europ...
The SUPRA research project – Simulation of Upset Recovery in Aviation – has been funded by the Europ...
The SUPRA research project - Simulation of Upset Recovery in Aviation - has been funded by the Europ...
The SUPRA research project – Simulation of Upset Recovery in Aviation – has been funded by the Europ...
The European research project SUPRA (“Simulation of Upset Recovery in Aviation”) produced an extende...
The collaborative research project SUPRA, intends to develop methodologies and advanced flight simul...
The paper presents the aerodynamic model in extended flight envelope for a generic airliner with und...
One of the primary objectives of the European Union 7th Framework Program research project SUPRA – “...
Aircraft departing from the nominal flight envelop and entering upset situations have become a major...
Currently, it is uncertain how well a typical ground-based simulator's hexapod motion system can sim...
Unsuccessful recovery from unusual flight attitudes, or airplane upset, is considered an important f...
The aim of the collaborative European research project ‘Simulation of UPset Recovery in Aviation’ (S...
Loss-of-control resulting from airplane upset is a leading cause of worldwide commercial aircraft ac...
The aerodynamic model of a generic airliner configuration is developed for a wide range of angles of...