Fault Detection and Isolation in Attitude and Heading Reference Systems For Fly-By-Wire Control System For General Aviation Aircraft 2006-01-2415
The article presents problems of fault detection and isolation in AHRS systems for the Fly-By-Wire control system for general aviation. The system is currently being designed at the Rzeszów University of Technology. The idea of the system is to create a general aviation pilot-friendly aircraft. The FBW control system is equipped with three AHRSs. Their diagnostics is realized on three levels. The article describes hardware redundancy and software redundancy for AHRS systems and then shows how to use it for diagnostics. The article focuses especially on estimation techniques applied in research. For simulations data from flight tests were used.
Citation: Kopecki, G. and Dolega, B., "Fault Detection and Isolation in Attitude and Heading Reference Systems For Fly-By-Wire Control System For General Aviation Aircraft," SAE Technical Paper 2006-01-2415, 2006, https://doi.org/10.4271/2006-01-2415. Download Citation
Grzegorz Kopecki, Boguslaw Dolega
Rzeszow University of Technology
General Aviation Technology Conference & Exhibition