Fault Detection and Isolation in Attitude and Heading Reference Systems For Fly-By-Wire Control System For General Aviation Aircraft

Author(s):  
Grzegorz Kopecki ◽  
Boguslaw Dolega
Aviation ◽  
2010 ◽  
Vol 14 (4) ◽  
pp. 112-116
Author(s):  
Tomasz Rogalski

This paper presents a conception of an airborne control system that can increase the safety of a general aviation aircraft. Sample threats appear on board the general aviation airplane discussed in the paper. The system monitors some events and flight parameters in the cockpit and can take some actions protecting the plane against threats if recognised as necessary. The paper presents sample actions fly‐by‐wire control systems can take to protect a plane against some threats on board. The system can modify a pilot's controls to correct flight and if it is not enough the system can disengage the pilot to autonomously fly the plane to the nearest safe airport Santrauka Straipsnyje pateikta valdymo iš oro sistemos koncepcija, kuri gali padidinti bendrosios aviacijos orlaiviu sauguma bei aptartos pavyzdines gresmes bendrosios aviacijos orlaiviuose. Aprašoma sistema stebi lakūno kabinoje rodomus ivairius skrydžio parametrus ir, kilus bet kokiai gresmei orlaivio saugumui, gali ji apsaugoti. Darbe pateikiami ir kompiuterizuoto elektrodistancinio valdymo sistemos pavyzdžiai, kurie taip pat gali apsaugoti orlaivi nuo jam kylančiu gresmiu. Ši sistema gali modifikuoti piloto valdyma taip, kad būtu pakoreguotas skrydis, o jei ir to neužtenka – sistema pajegi ir autonominiam skrydžiui, kuomet orlaivis yra nukreipiamas i artimiausia ir saugiausia oro uosta be piloto pagalbos.


Sign in / Sign up

Export Citation Format

Share Document