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.
| Original language | English |
|---|---|
| Pages (from-to) | 34-42 |
| Number of pages | 9 |
| Journal | Aerospace Science and Technology |
| Volume | 23 |
| Issue number | 1 |
| DOIs | |
| State | Published - Dec 2012 |
| Externally published | Yes |
Keywords
- Flight mechanics
- Optimal control
- Rotorcraft vehicles
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