Article ID | Journal | Published Year | Pages | File Type |
---|---|---|---|---|
8057267 | Aerospace Science and Technology | 2018 | 8 Pages |
Abstract
This research presents a nonlinear gain-scheduled flight controller design method via a stable manifold theory in order to handle the nonlinearities of the F-18 High Alpha Research Vehicle due to the change in the aerodynamic characteristics at different angles of attack and the airspeed variation. The designed longitudinal flight control system consists of a nonlinear gain-scheduled stabilization augmentation system which is designed using the stable manifold method, and a linear gain-scheduled control augmentation system which consists of proportional and integral gains. The nonlinear longitudinal flight controller is verified in a 6 degree-of-freedom simulator.
Related Topics
Physical Sciences and Engineering
Engineering
Aerospace Engineering
Authors
Anh Tuan Tran, Noboru Sakamoto, Koichi Mori,