Elaboration of Simulation Complex for Realization of Adaptive Neural Flight Control System to be used on Commercial Aircraft in Compliance with EASA-FAA Standards

• Autorzy: Prosvirin Dmytro , Pawęska Marcin , Kharchenko Volodymyr

Identyfikatory

DOI

10.26411/83-1734-2015-2-56-15-24

• Języki publikacji: EN

Abstrakty

EN

In this paper, the typical scheme of the adaptive neuron technology of automatic control systems (ACS) of aircraft, which is adhered to by all the main developers of control systems, is considered. The theoretical justification of the current tendencies of reducing the volume of flight tests by increasing the volume of mathematical modelling and bench testing has been given.

Słowa kluczowe

EN

Automatic flight control system; ACS; mathematical modelling; simulation; visualization

• Wydawca: Międzynarodowa Wyższa Szkoła Logistyki i Transportu we Wrocławiu
• Czasopismo: Logistics and Transport
• Rocznik: 2024
• Tom: Vol. 61-62, No. 1-2
• Strony: 105--113
• Opis fizyczny: Bibliogr. 10 poz., rys.

Twórcy

autor

Prosvirin Dmytro

• Air Navigation Department, National Aviation University, ANTONOV Company Kyiv, Ukraine

• https://orcid.org/0000-0002-1336-8731

autor

Pawęska Marcin

• The International University Logistic and Transport in Wroclaw

• https://orcid.org/0000-0002-6728-2423

autor

Kharchenko Volodymyr

• Airspace Centre, National Aviation University, Kyiv, Ukraine

• https://orcid.org/0000-0001-7575-4366

Bibliografia

• [1] Software considerations in airborne systems and equipment certification (RTCA/DO- 178B): DO-178B- [December 1. 1992]. - Washington. D.C. 20036 USA, 1992, p. 112.
• [2] Efficient Development of Safe Avionics Display Software with DO-178B Objectives Using SCADE Suite™: [Methodology Handbook]. - France: Esterel Technologies, 2012, p. 110.
• [3] Shligerski A., Model-based development of safe application software for safety-critical railways systems using scade tool environment. Shligerski A., Umanski V.-M.: “Functional safety – theory and practice”, 2009, pp.13-21.
• [4] RTCA DO-178C Software Considerations in Airborne Systems and Equipment Certification, RTCA, Inc. Washington, DC USA, December 13, 2011.
• [5] RTCA DO-254 Design Assurance Guidance for Airborne Electronic Hardware ©, RTCA, Inc. Washington DC, USA, April 19, 2000.
• [6] RTCA DO-330 Software Tool Qualification Considerations, RTCA, Inc. Washington DC USA, December 13, 2011.
• [7] RTCA DO-331 Model-Based Development and Verification Supplement to DO-178C and DO-278A, RTCA, Inc. Washington DC, USA, December 13, 2011.
• [8] RTCA DO-332 Object-Oriented Technology and Related Techniques Supplement to DO-178C and DO-278A, RTCA, Inc. Washington DC, USA, December 13, 2011.
• [9] D. Prosvirin, V. Kharchenko, IMPROVEMENT OF “AIRCRAFT-AUTOMATIC FLIGHT CONTROL SYSTEM” CONTROL LOOP QUALITY. Electronics and Control Systems, DOI: 10.18372/1990-5548.47.10265, 2016.
• [10] https://www.researchgate.net/publication/315506757_IMPROVEMENT_OF_ AIRCRAFT-AUTOMATIC_FLIGHT_CONTROL_SYSTEM_CONTROL_LOOP_ QUALITY