This presentation describes a model-predictive automatic recovery system for aircraft on the verge of a loss-of-control situation. The system determines when it must intervene to prevent an imminent accident, resulting from a poor approach. It estimates the altitude loss that would result from a go-around maneuver at the current flight condition. If the loss is projected to violate a minimum altitude threshold, the maneuver is automatically triggered. The system deactivates to allow landing once several criteria are met. Piloted flight simulator evaluation showed the system to provide effective envelope protection during extremely unsafe landing attempts. The results demonstrate how flight and propulsion control can be integrated to recover...
Autonomous contingency management systems, such as a forced landing system which reacts appropriatel...
A piloted simulator investigation of various engine failure compensation concepts for powered-lift S...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/83594/1/AIAA-2010-3353-745.pd
This paper describes a model-predictive automatic recovery system for aircraft on the verge of a los...
In recent studies, it has been observed that loss of control in flight is the most frequent primary ...
This project examined the application of intelligent cockpit systems to aid air transport pilots at ...
Flying near the edge of the safe operating envelope is an inherently unsafe proposition. Edge of the...
Increasingly autonomous (IA) systems support aircraft flight crews in all tasks required for safe em...
In this paper we present a technique for approximating the short-period dynamics of an exploration-c...
Small Unmanned Aircraft Systems (UAS) are considered the stepping stone for the integration of civil...
Slides for an invited presentation (as part of a series) at Santa Clara University, invited by prof....
Pilot-activated automatic recovery systems (PARS) are a common feature of combat aircraft and are us...
The coupling of expert systems and control design and analysis techniques are documented to provide ...
Effective and safe control of an aircraft may be difficult or nearly impossible for a pilot followin...
Although today's aircraft provide a safe and reliable form of transportation, in this era of string...
Autonomous contingency management systems, such as a forced landing system which reacts appropriatel...
A piloted simulator investigation of various engine failure compensation concepts for powered-lift S...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/83594/1/AIAA-2010-3353-745.pd
This paper describes a model-predictive automatic recovery system for aircraft on the verge of a los...
In recent studies, it has been observed that loss of control in flight is the most frequent primary ...
This project examined the application of intelligent cockpit systems to aid air transport pilots at ...
Flying near the edge of the safe operating envelope is an inherently unsafe proposition. Edge of the...
Increasingly autonomous (IA) systems support aircraft flight crews in all tasks required for safe em...
In this paper we present a technique for approximating the short-period dynamics of an exploration-c...
Small Unmanned Aircraft Systems (UAS) are considered the stepping stone for the integration of civil...
Slides for an invited presentation (as part of a series) at Santa Clara University, invited by prof....
Pilot-activated automatic recovery systems (PARS) are a common feature of combat aircraft and are us...
The coupling of expert systems and control design and analysis techniques are documented to provide ...
Effective and safe control of an aircraft may be difficult or nearly impossible for a pilot followin...
Although today's aircraft provide a safe and reliable form of transportation, in this era of string...
Autonomous contingency management systems, such as a forced landing system which reacts appropriatel...
A piloted simulator investigation of various engine failure compensation concepts for powered-lift S...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/83594/1/AIAA-2010-3353-745.pd