The aircraft minimum time-to-climb problem has been treated by many investigators. But many of these studies have been concerned primarily with the development of improved numerical techniques for solving the minimum time-to-climb problem. Often, various numerical methods are applied to a specific aircraft dynamic model, and the corresponding results are compared to reveal the relative advantages and disadvantages of the methods. In this paper, five dynamic models are examined. The models used range from the simple energy-state model to the complete point-mass model with five state variables. The primary objective is to compare the solutions for each of these five models with regard to accuracy and computational effort. Numerical results are presented for an early represention of the F-4 fighter aircraft.
Aircraft minimum time-to-climb model comparison
Vergleich von Modellen zur Bestimmung der minimalen Steigzeit von Flugzeugen
1987
10 Seiten, 5 Bilder, 1 Tabelle, 19 Quellen
Aufsatz (Konferenz)
Englisch
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