Fault Detection and Fail-Safe Operation with a Multiple-Redundancy Air-Data System
- Eubank, Ryan
- Atkins, Ella
- Ogura, Stephanie
DOIAbstract
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/83640/1/AIAA-2010-7855-622.pd
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/83640/1/AIAA-2010-7855-622.pd
The aim of this thesis is to design a fault detection and accommodation (FDA) algorithm for air data...
The aim of the air data system, in a full-authority fly-by-wire control system, is the determination...
The presence of failures in navigation sensors can cause the determination of an erroneous aircraft ...
University of Minnesota M.S. thesis. Major: Aerospace engineering and mechanics. Advisors: Gary J. B...
Abstract: Air data probes provide essential sensing capabilities to aircraft. The loss or corruption...
Although very uncommon, the sequential failures of all aircraft Pitot tubes, with the consequent los...
The design of a sensor fault tolerant system which uses analytical redundancy for the Terminal Confi...
This paper presents a redundant-sensor-based adaptive Fault Detection and Isolation (FDI) algorithm,...
In the modern world, systems such as aircraft systems are becoming increasingly complex, often consi...
Unmanned Airborne Vehicles (UAV) are assuming prominent roles in both the commercial and military ae...
A method for failure detection and isolation (FDI) for redundant aircraft sensors is presented. The ...
Abstract: System redundancy in aircraft is very important as it ensures faulty components would not ...
ITC/USA 2010 Conference Proceedings / The Forty-Sixth Annual International Telemetering Conference a...
Abstract — In the aircraft industry, it is common to use physically redundant components to ensure t...
To maintain nominal flight control system functionalities during fault scenarios, enhancements of th...
The aim of this thesis is to design a fault detection and accommodation (FDA) algorithm for air data...
The aim of the air data system, in a full-authority fly-by-wire control system, is the determination...
The presence of failures in navigation sensors can cause the determination of an erroneous aircraft ...
University of Minnesota M.S. thesis. Major: Aerospace engineering and mechanics. Advisors: Gary J. B...
Abstract: Air data probes provide essential sensing capabilities to aircraft. The loss or corruption...
Although very uncommon, the sequential failures of all aircraft Pitot tubes, with the consequent los...
The design of a sensor fault tolerant system which uses analytical redundancy for the Terminal Confi...
This paper presents a redundant-sensor-based adaptive Fault Detection and Isolation (FDI) algorithm,...
In the modern world, systems such as aircraft systems are becoming increasingly complex, often consi...
Unmanned Airborne Vehicles (UAV) are assuming prominent roles in both the commercial and military ae...
A method for failure detection and isolation (FDI) for redundant aircraft sensors is presented. The ...
Abstract: System redundancy in aircraft is very important as it ensures faulty components would not ...
ITC/USA 2010 Conference Proceedings / The Forty-Sixth Annual International Telemetering Conference a...
Abstract — In the aircraft industry, it is common to use physically redundant components to ensure t...
To maintain nominal flight control system functionalities during fault scenarios, enhancements of th...
The aim of this thesis is to design a fault detection and accommodation (FDA) algorithm for air data...
The aim of the air data system, in a full-authority fly-by-wire control system, is the determination...
The presence of failures in navigation sensors can cause the determination of an erroneous aircraft ...
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