Optimal Flight for Ground Noise Reduction in Helicopter Landing Approach: Optimal Altitude and Velocity Control

This study aims to obtain the optimal flights of a helicopter that reduce ground noise during landing approach with an optimization technique, and to conduct flight tests for confirming the effectiveness of the optimal solutions. Past experiments of Japan Aerospace Exploration Agency (JAXA) show tha...

Ausführliche Beschreibung

Bibliographische Detailangaben

Veröffentlicht in:	Transactions of the Japan Society for Aeronautical and Space Sciences 2007-11, Vol.49 (169), p.209-217
Hauptverfasser:	Tsuchiya, Takeshi, Ishii, Hirokazu, Uchida, Junichi, Gomi, Hiromi, Matayoshi, Naoki, Okuno, Yoshinori
Format:	Artikel
Sprache:	eng
Online-Zugang:	Volltext
Tags:	Tag hinzufügen Keine Tags, Fügen Sie den ersten Tag hinzu!