Matches in SemOpenAlex for { <https://semopenalex.org/work/W4311185923> ?p ?o ?g. }
Showing items 1 to 82 of
82
with 100 items per page.
- W4311185923 endingPage "181" @default.
- W4311185923 startingPage "167" @default.
- W4311185923 abstract "To accurately predict the amount of fuel needed by an aircraft for a given flight, a performance model must account for engine and airframe degradation. This paper presents a methodology to identify an aero-propulsive model to predict the fuel flow of an aircraft in cruise, while considering initial modeling uncertainties and performance variation over time due to degradation. Starting from performance data obtained from a Research Aircraft Flight Simulator, an initial aero-propulsive model was identified using different estimation methods. The estimation methods studied in this paper were polynomial interpolation, thin-plate splines, and neural networks. The aero-propulsive model was then structured using two lookup tables: one lookup table reflecting the aerodynamic performance, and another table reflecting the propulsive performance. Subsequently, an adaptative technique was developed to locally and then globally, adapt the lookup tables defining the aero-propulsive model using flight data. The methodology was applied to the Cessna Citation X business jet aircraft, for which a highly qualified level D research aircraft flight simulator was available. The results demonstrated that by using the proposed aero-propulsive performance model, it was possible to predict the aerodynamic performance with an average relative error of 0.99%, and the propulsive performance with an average relative error of 3.38%. These results were obtained using the neural network estimation method." @default.
- W4311185923 created "2022-12-24" @default.
- W4311185923 creator A5006804321 @default.
- W4311185923 creator A5051429851 @default.
- W4311185923 creator A5052427970 @default.
- W4311185923 date "2022-12-02" @default.
- W4311185923 modified "2023-10-16" @default.
- W4311185923 title "Development of an Adaptive Aero-Propulsive Performance Model in Cruise Flight – Application to the Cessna Citation X" @default.
- W4311185923 cites W1966314190 @default.
- W4311185923 cites W2001662718 @default.
- W4311185923 cites W2766453766 @default.
- W4311185923 cites W2872292047 @default.
- W4311185923 cites W2954561314 @default.
- W4311185923 cites W2968625968 @default.
- W4311185923 cites W2995097341 @default.
- W4311185923 cites W3022678419 @default.
- W4311185923 cites W3112982658 @default.
- W4311185923 cites W3135245267 @default.
- W4311185923 cites W4280591100 @default.
- W4311185923 cites W48783140 @default.
- W4311185923 doi "https://doi.org/10.13111/2066-8201.2022.14.4.14" @default.
- W4311185923 hasPublicationYear "2022" @default.
- W4311185923 type Work @default.
- W4311185923 citedByCount "0" @default.
- W4311185923 crossrefType "journal-article" @default.
- W4311185923 hasAuthorship W4311185923A5006804321 @default.
- W4311185923 hasAuthorship W4311185923A5051429851 @default.
- W4311185923 hasAuthorship W4311185923A5052427970 @default.
- W4311185923 hasBestOaLocation W43111859231 @default.
- W4311185923 hasConcept C127413603 @default.
- W4311185923 hasConcept C13393347 @default.
- W4311185923 hasConcept C134835016 @default.
- W4311185923 hasConcept C146978453 @default.
- W4311185923 hasConcept C154945302 @default.
- W4311185923 hasConcept C199360897 @default.
- W4311185923 hasConcept C205167488 @default.
- W4311185923 hasConcept C2778821358 @default.
- W4311185923 hasConcept C2781407631 @default.
- W4311185923 hasConcept C41008148 @default.
- W4311185923 hasConcept C41376638 @default.
- W4311185923 hasConcept C42021957 @default.
- W4311185923 hasConcept C44154836 @default.
- W4311185923 hasConcept C45882903 @default.
- W4311185923 hasConcept C50644808 @default.
- W4311185923 hasConcept C79420006 @default.
- W4311185923 hasConceptScore W4311185923C127413603 @default.
- W4311185923 hasConceptScore W4311185923C13393347 @default.
- W4311185923 hasConceptScore W4311185923C134835016 @default.
- W4311185923 hasConceptScore W4311185923C146978453 @default.
- W4311185923 hasConceptScore W4311185923C154945302 @default.
- W4311185923 hasConceptScore W4311185923C199360897 @default.
- W4311185923 hasConceptScore W4311185923C205167488 @default.
- W4311185923 hasConceptScore W4311185923C2778821358 @default.
- W4311185923 hasConceptScore W4311185923C2781407631 @default.
- W4311185923 hasConceptScore W4311185923C41008148 @default.
- W4311185923 hasConceptScore W4311185923C41376638 @default.
- W4311185923 hasConceptScore W4311185923C42021957 @default.
- W4311185923 hasConceptScore W4311185923C44154836 @default.
- W4311185923 hasConceptScore W4311185923C45882903 @default.
- W4311185923 hasConceptScore W4311185923C50644808 @default.
- W4311185923 hasConceptScore W4311185923C79420006 @default.
- W4311185923 hasIssue "4" @default.
- W4311185923 hasLocation W43111859231 @default.
- W4311185923 hasLocation W43111859232 @default.
- W4311185923 hasOpenAccess W4311185923 @default.
- W4311185923 hasPrimaryLocation W43111859231 @default.
- W4311185923 hasRelatedWork W2264394166 @default.
- W4311185923 hasRelatedWork W2335054725 @default.
- W4311185923 hasRelatedWork W2370595353 @default.
- W4311185923 hasRelatedWork W30013722 @default.
- W4311185923 hasRelatedWork W3085131070 @default.
- W4311185923 hasRelatedWork W3128421326 @default.
- W4311185923 hasRelatedWork W4245531100 @default.
- W4311185923 hasRelatedWork W4379930089 @default.
- W4311185923 hasRelatedWork W752094364 @default.
- W4311185923 hasRelatedWork W819440923 @default.
- W4311185923 hasVolume "14" @default.
- W4311185923 isParatext "false" @default.
- W4311185923 isRetracted "false" @default.
- W4311185923 workType "article" @default.