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A Proposal for a Fully Distributed Flight Control System Design (CROSBI ID 637522)

Prilog sa skupa u zborniku | izvorni znanstveni rad | međunarodna recenzija

Šegvić, Miroslav ; Krajček Nikolić, Karolina ; Ivanjko, Edouard A Proposal for a Fully Distributed Flight Control System Design // Proceedings of 39th International Convention MIPRO2016 / Biljanović, Petar (ur.). Rijeka: Hrvatska udruga za informacijsku i komunikacijsku tehnologiju, elektroniku i mikroelektroniku - MIPRO, 2016. str. 1306-1310 doi: 10.1109/MIPRO.2016.7522304

Podaci o odgovornosti

Šegvić, Miroslav ; Krajček Nikolić, Karolina ; Ivanjko, Edouard

engleski

A Proposal for a Fully Distributed Flight Control System Design

Since the delivery of the first A320 airliner with a Fly-by-Wire Flight Control System (FCS) in 1988, aircraft avionics architecture evolved significantly. Federated Architecture applied in the A320 family of aircraft presumed one computer per function. Limits regarding weight and space availability were reached and new generation of aircraft designed in early 2000s were equipped with Distributed Integrated Modular Avionics Architecture consisting of shared hardware resources running separate software modules according to aircraft priorities. Flight Control Computer functions were assumed by the Flight Control Module. While reducing the cost, weight and number of computers on board the aircraft, problems with troubleshooting and system modifications emerged. Proving that critical Systems perform within certain certification safety requirements became infeasible due to unpredictable dependencies between software modules. Abovementioned problems are addressed in this paper with a proposal of a Fully Distributed Flight Control System (FDFCS) design. Main contribution is that aircraft stability and trajectory control logic is distributed to a network of independent Control Units (CU) collocated on actuators collaborating to control the aircraft with respect to common goal. This paper outlines design for FDFCS and its CUs. Problems that distributed FCS implies and solves are identified. Finally, requirements for planned FDFCS Hardware in the Loop Simulator are set.

Flight control system ; distributed control ; integrated modular avionics architecture

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Podaci o prilogu

1306-1310.

2016.

objavljeno

10.1109/MIPRO.2016.7522304

Podaci o matičnoj publikaciji

Proceedings of 39th International Convention MIPRO2016

Biljanović, Petar

Rijeka: Hrvatska udruga za informacijsku i komunikacijsku tehnologiju, elektroniku i mikroelektroniku - MIPRO

978-953-233-087-8

Podaci o skupu

MIPRO 2016

predavanje

30.05.2016-03.06.2016

Opatija, Hrvatska

Povezanost rada

Elektrotehnika, Tehnologija prometa i transport, Zrakoplovstvo, raketna i svemirska tehnika

Poveznice
Indeksiranost