Over the years gradually flight management systems have been added to airplanes which reduce pilot workload and increase safety. These systems however do not provide an adequate response when in an emergency situation the aircraft loses all thrust. A system that creates glide trajectories to airports that are reachable would enable pilots to focus their attention on stabilizing and regaining control in an in-flight emergency situation. The objective of this study is to develop such an emergency flight system that can generate glide trajectories from the position at which the emergency starts to all reachable runways. By first determining the maximum range of the aircraft, a footprint is defined in which the reachable runways are identified....
Current Flight Management Systems (FMS) can autonomously fly an aircraft from takeoff through landin...
International audienceAircraft total failure of engines or engine-out, is a dramatic situation which...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/77332/1/AIAA-2007-6873-998.pd
We present an automated emergency trajectory generator to compute the best emergency trajectory for ...
We present an automated emergency trajectory generator to compute the best emergency trajectory for ...
Increasingly autonomous (IA) systems support aircraft flight crews in all tasks required for safe em...
We present an automated emergency trajectory generator to compute the best emergency trajectory for ...
We present an automated emergency trajectory generator to compute the best emergency trajectory for ...
International audienceThe purpose of this communication is to contribute to the development of a new...
Unmanned aircraft must be characterized by a level of safety, similar to that of manned aircraft, wh...
AbstractEmergency flight path planning process was established for the failure of total loss of thru...
International audienceIn this paper, an efficient algorithm to generate a short and safe trajectory ...
Engine-out is an undoubted critical situation for flight safety. The objective of this thesis is to ...
By the year 2020 the number of aircraft will have increased substantially and will be in 'Free Fligh...
In this paper, we present the development of a system for automation of the emergency maneuver for a...
Current Flight Management Systems (FMS) can autonomously fly an aircraft from takeoff through landin...
International audienceAircraft total failure of engines or engine-out, is a dramatic situation which...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/77332/1/AIAA-2007-6873-998.pd
We present an automated emergency trajectory generator to compute the best emergency trajectory for ...
We present an automated emergency trajectory generator to compute the best emergency trajectory for ...
Increasingly autonomous (IA) systems support aircraft flight crews in all tasks required for safe em...
We present an automated emergency trajectory generator to compute the best emergency trajectory for ...
We present an automated emergency trajectory generator to compute the best emergency trajectory for ...
International audienceThe purpose of this communication is to contribute to the development of a new...
Unmanned aircraft must be characterized by a level of safety, similar to that of manned aircraft, wh...
AbstractEmergency flight path planning process was established for the failure of total loss of thru...
International audienceIn this paper, an efficient algorithm to generate a short and safe trajectory ...
Engine-out is an undoubted critical situation for flight safety. The objective of this thesis is to ...
By the year 2020 the number of aircraft will have increased substantially and will be in 'Free Fligh...
In this paper, we present the development of a system for automation of the emergency maneuver for a...
Current Flight Management Systems (FMS) can autonomously fly an aircraft from takeoff through landin...
International audienceAircraft total failure of engines or engine-out, is a dramatic situation which...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/77332/1/AIAA-2007-6873-998.pd