Computer Based Performance Analysis with Substitution Functions

doi: 10.32560/rk.2022.1.7

Abstract

The methods used so far and adopted by the Authority have been a huge effort to select results (in most cases performance-limited mass values) from discrete value sets generated under specified boundary conditions at separate phases of flight. In the best case, the resulting values were analysed by algorithms that gave the operator the most important value for the ATL, given the MATOM and OM for the task. Taking these into account, a sophisticated solution should also help to prepare the load documentation. 

Keywords:

aircraft engine failure accessibility performance analysis functions approximation mass limits

How to Cite

[1]
D. Szilágyi, “Computer Based Performance Analysis with Substitution Functions”, RepTudKoz, vol. 34, no. 1, pp. 111–127, Nov. 2022.

References

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[2] Beechcraft BE-76 Pilot Operating Handbook. pp. 5–26. 1978.

[3] 965/2012 EU rendelet 17. módosítása, 2022. Online: https://www.easa.europa.eu/document-library/easy-access-rules/easy-access-rules-air-operations-regulation-eu-no-9652012

[4] Kormos Á., Számítógépes teljesítmény-analízis készítése BE76 típusú repülőgépre és CAT/NCO műveletekre. Szakdolgozat. Nyíregyházi Egyetem, 2021.

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