| Article ID | Journal | Published Year | Pages | File Type |
|---|---|---|---|---|
| 1718345 | Aerospace Science and Technology | 2012 | 9 Pages |
Abstract
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 maneuver 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.
Keywords
Related Topics
Physical Sciences and Engineering
Engineering
Aerospace Engineering
Authors
Carlo L. Bottasso, Fabio Luraghi, Giorgio Maisano,