| Article ID | Journal | Published Year | Pages | File Type |
|---|---|---|---|---|
| 716118 | IFAC Proceedings Volumes | 2010 | 6 Pages |
Abstract
This paper introduces the dynamic inversion with the Lyapunov function method. This is for a guidance and control system of a chase UAV with the velocity controller which is designed based on a dynamic inversion approach. The guidance and control system employs the pure pursuit guidance to determine the UAV's orientation, and a two-time scale dynamic inversion technique to control the attitude. All together, they enable the UAV to keep formation flight.
Related Topics
Physical Sciences and Engineering
Engineering
Computational Mechanics
