C.L. Bottasso, G. Maisano, F. Luraghi

The present paper focuses on trajectory optimization problems for complex first-principle models of rotorcraft vehicles, accounting for the presence of slow and fast dynamic components in the solution. The trajectory optimal control problem is solved through a direct approach by means of a novel hybrid single-multiple shooting method. The capabilities of the proposed procedures are illustrated with the help of an application regarding the estimation of the H-V diagram of a tilt-rotor.

35th European Rotorcraft Forum 2009,

Conference Paper

englisch

21,0 x 29,7 cm, 13 Seiten

DGLR-Bericht, 2009, 2009-03, 35th European Rotorcraft Forum 2009 - Conference Proceedings; S.1-13; 2009; Deutsche Gesellschaft für Luft- und Raumfahrt - Lilienthal-Oberth e.V., Bonn

NA

in getr. Zählung;

control input, rotorcrafts

Bestellbar

2009