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Flight path optimization problems related to vehicle fixed thrust direction

  • Institute of Flight Mechanics and Flight Control
  • Technische Universität München

Publikation: KonferenzbeitragPapierBegutachtung

1 Zitat (Scopus)

Abstract

A problem in airplane performance optimization concerns the modelling of the thrust force direction. There are fundamental optimality difficulties when the thrust force is considered fixed on the vehicle. An approach is presented which is capable of producing a solution for the above problem. A relaxed optimization problem is constructed as an equivalent of the original system and a solution is developed on this basis. A range cruise problem of hypersonic flight is used as a numerical example.

OriginalspracheEnglisch
Seiten1-9
Seitenumfang9
PublikationsstatusVeröffentlicht - 1996
VeranstaltungGuidance, Navigation, and Control Conference and Exhibit, 1996 - San Diego, USA/Vereinigte Staaten
Dauer: 29 Juli 199631 Juli 1996

Konferenz

KonferenzGuidance, Navigation, and Control Conference and Exhibit, 1996
Land/GebietUSA/Vereinigte Staaten
OrtSan Diego
Zeitraum29/07/9631/07/96

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