This paper presents a redundant-sensor-based Fault Detection and Isolation (FDI) algorithm, applied to a receiver aircraft in aerial refueling operation. The FDI algorithm is based on a statistical approach and uses measurements from three identical airdata sensors placed at different locations. The airdata sensors measure airspeed, angle-of-attack, and side slip angle. Simulation results show that the FDI algorithm successfully performs detection and isolation of sensor faults when the receiver aircraft flies solo or outside the wake of the tanker aircraft. However, simulation experiments also show that the FDI algorithm yields false fault detection when the receive aircraft flies within the nonuniform wind field, induced by the wake vortices of the tanker.
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Details
Title
False fault detection in airdata sensor due to nonuniform wind in aerial refueling
Publication Details
AIAA Atmospheric Flight Mechanics Conference
Resource Type
Conference proceeding
Conference
AIAA Atmospheric Flight Mechanics Conference ( Portland, USA, 08/08/2011–08/11/2011)
Publisher
American Institute of Aeronautics and Astronautics, Inc.; United States
Copyright
2011 by Atilla Dogan
Identifiers
99380090305806600
Academic Unit
Intelligent Systems and Robotics; Hal Marcus College of Science and Engineering