| Article ID | Journal | Published Year | Pages | File Type |
|---|---|---|---|---|
| 712466 | IFAC-PapersOnLine | 2015 | 5 Pages |
Abstract
The paper describes the problem of adaptive control of the aircraft lateral movement in landing mode. The control system with a reference model based on the modified algorithm of high order tuner is proposed. The proposed algorithm tracks the output of the plant to the reference output with the required accuracy. Simulation results illustrate the efficiency of the synthesized algorithm.
Related Topics
Physical Sciences and Engineering
Engineering
Computational Mechanics
