Minimum Time Turn of a Helicopter

Using a point mass approximation, two and three dimensional minimum time turn problems of a helicopter are formulated as the nonlinear optimal control problems. Optimum solutions are obtained numerically by SCGRA and MQA. The rotor is modeled as an ideal aerodynamic force generator which provide the...

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Bibliographische Detailangaben

Veröffentlicht in:	Aeronautical and Space Sciences Japan 1993/05/05, Vol.41(472), pp.293-299
Hauptverfasser:	NEKOHASHI, Toshifumi, SASAKI, Shigeru, NAGASHIMA, Tomoari
Format:	Artikel
Sprache:	jpn
Schlagworte:	Flight Dynamics Helicopters Maneuverability
Online-Zugang:	Volltext
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