Aircraft vertical profile implementation using directed-graph methods
Aircraft vertical profile implementation using directed-graph methods
- New search for: Brewster, L.T.
- New search for: Stigall, P.D.
- New search for: Brewster, L.T.
- New search for: Stigall, P.D.
Aircraft vertical profile simulation is realized using a demand-driven minimal-calculation directed graph structure to reduce calculation time and to force synchronization of the performance measurement functions with the system state variables. Performance-directed model adaptation makes dynamic vertical profile path corrections, in the presence of fixed drag variations, possible. Drag variations ranging from +10% to -10% yielded fuel consumption improvements of less than 1% in the majority of the cases. Calculation time improvement for path simulation ranges from a factor of 1.19 in the worst case to 1.5 in the best case.
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Aircraft vertical profile implementation using directed-graph methods
Die Implementierung der vertikalen Profil-Simulation bei Flugzeugen mit der Methode der gerichteten Graphen
IEEE Transactions on Aerospace and Electronic Systems ; 24 , 6 ; 682-692
1988
11 Seiten, 17 Quellen
Article (Journal)
English
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