| Article ID | Journal | Published Year | Pages | File Type |
|---|---|---|---|---|
| 5003036 | IFAC-PapersOnLine | 2016 | 6 Pages |
Abstract
In this paper, a multi-objective optimization-based methodology for rotorcraft attitude control law design is applied to a tilt-rotor case; the framework allows to enforce requirements of stability, performance, control action moderation, and safety. The structured Hâ approach is taken into account, and the optimization problem is stated as a mixed-sensitivity problem. Rotor state feedback is used to limit flap motion, and is introduced as an additional loop to a classical attitude control law.
Related Topics
Physical Sciences and Engineering
Engineering
Computational Mechanics
Authors
S. Panza, L. Guastalla, B. Roda, M. Lovera,