Zusammenfassung
Die Grundgleichungen (1.6.17) beschreiben in allgemeiner Form die Flugbahn eines Luftfahrzeugs unter der Einwirkung von aerodynamischen, Antriebs- und Gewichtskräften. Sind diese Kräfte unausgeglichen, so werden zusätzliche Trägheitskräfte wirksam; Betrag und/oder Richtung des Geschwindigkeitsvektors sind dann zeitlich veränderliche Größen. Zur Bestimmung der Flugbahn in konkreten Fällen müssen die Grundgleichungen — ein System von Differentialgleichungen — integriert werden. Diese Aufgabe ist nur in einfachen Sonderfällen analytisch lösbar, da einige der in den Grundgleichungen enthaltenen Größen nichtlinear von den Zustandsgrößen V, γ und H abhängen und unter Umständen nur in der Form von Kurvenoder Tabellen bekannt sind.
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Brüning, G., Hafer, X., Sachs, G. (1986). Flugzustände. In: Flugleistungen. Hochschultext. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-662-07259-2_3
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