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Pregled bibliografske jedinice broj: 826063

A Proposal for a Fully Distributed Flight Control System Design


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 (predavanje, međunarodna recenzija, cjeloviti rad (in extenso), znanstveni)


CROSBI ID: 826063 Za ispravke kontaktirajte CROSBI podršku putem web obrasca

Naslov
A Proposal for a Fully Distributed Flight Control System Design

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

Vrsta, podvrsta i kategorija rada
Radovi u zbornicima skupova, cjeloviti rad (in extenso), znanstveni

Izvornik
Proceedings of 39th International Convention MIPRO2016 / Biljanović, Petar - Rijeka : Hrvatska udruga za informacijsku i komunikacijsku tehnologiju, elektroniku i mikroelektroniku - MIPRO, 2016, 1306-1310

ISBN
978-953-233-087-8

Skup
39th International Convention MIPRO2016

Mjesto i datum
Opatija, Hrvatska, 30.05.2016. - 03.06.2016

Vrsta sudjelovanja
Predavanje

Vrsta recenzije
Međunarodna recenzija

Ključne riječi
Flight control system ; distributed control ; integrated modular avionics architecture

Sažetak
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.

Izvorni jezik
Engleski

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



POVEZANOST RADA


Ustanove:
Fakultet prometnih znanosti, Zagreb

Poveznice na cjeloviti tekst rada:

doi

Citiraj ovu publikaciju:

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 (predavanje, međunarodna recenzija, cjeloviti rad (in extenso), znanstveni)
Šegvić, M., Krajček Nikolić, K. & Ivanjko, E. (2016) A Proposal for a Fully Distributed Flight Control System Design. U: Biljanović, P. (ur.)Proceedings of 39th International Convention MIPRO2016 doi:10.1109/MIPRO.2016.7522304.
@article{article, author = {\v{S}egvi\'{c}, Miroslav and Kraj\v{c}ek Nikoli\'{c}, Karolina and Ivanjko, Edouard}, editor = {Biljanovi\'{c}, P.}, year = {2016}, pages = {1306-1310}, DOI = {10.1109/MIPRO.2016.7522304}, keywords = {Flight control system, distributed control, integrated modular avionics architecture}, doi = {10.1109/MIPRO.2016.7522304}, isbn = {978-953-233-087-8}, title = {A Proposal for a Fully Distributed Flight Control System Design}, keyword = {Flight control system, distributed control, integrated modular avionics architecture}, publisher = {Hrvatska udruga za informacijsku i komunikacijsku tehnologiju, elektroniku i mikroelektroniku - MIPRO}, publisherplace = {Opatija, Hrvatska} }
@article{article, author = {\v{S}egvi\'{c}, Miroslav and Kraj\v{c}ek Nikoli\'{c}, Karolina and Ivanjko, Edouard}, editor = {Biljanovi\'{c}, P.}, year = {2016}, pages = {1306-1310}, DOI = {10.1109/MIPRO.2016.7522304}, keywords = {Flight control system, distributed control, integrated modular avionics architecture}, doi = {10.1109/MIPRO.2016.7522304}, isbn = {978-953-233-087-8}, title = {A Proposal for a Fully Distributed Flight Control System Design}, keyword = {Flight control system, distributed control, integrated modular avionics architecture}, publisher = {Hrvatska udruga za informacijsku i komunikacijsku tehnologiju, elektroniku i mikroelektroniku - MIPRO}, publisherplace = {Opatija, Hrvatska} }

Časopis indeksira:


  • Web of Science Core Collection (WoSCC)
    • SCI-EXP, SSCI i/ili A&HCI
    • Conference Proceedings Citation Index - Science (CPCI-S)
  • Scopus


Citati:





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