Abstract
We provide a global framework for flatness-based motion planning and dynamic feedback linearization of the quadcopter dynamics. It allows us to avoid the singularity difficulty that comes from the use of the yaw angle in flat output construction and dynamic feedback linearization. We construct eight differentially flat charts the union of which covers the entire configuration space of the quadcopter dynamics so that we can do global motion planning without encountering any singularity. In each differentially flat chart we transform the 12-dimensional quadcopter system via dynamic feedback to a 14-dimensional linear controllable system, which makes tracking controller design straightforward, so that we can switch from one controller to another to track a globally planned trajectory. The central theme of this paper is the global approach to the quadcopter motion planning and tracking.
| Original language | English |
|---|---|
| Title of host publication | 53rd IEEE Conference on Decision and Control,CDC 2014 |
| Publisher | Institute of Electrical and Electronics Engineers Inc. |
| Pages | 686-691 |
| Number of pages | 6 |
| Edition | February |
| ISBN (Electronic) | 9781479977468 |
| DOIs | |
| State | Published - 2014 |
| Event | 2014 53rd IEEE Annual Conference on Decision and Control, CDC 2014 - Los Angeles, United States Duration: 15 Dec 2014 → 17 Dec 2014 |
Publication series
| Name | Proceedings of the IEEE Conference on Decision and Control |
|---|---|
| Number | February |
| Volume | 2015-February |
| ISSN (Print) | 0743-1546 |
| ISSN (Electronic) | 2576-2370 |
Conference
| Conference | 2014 53rd IEEE Annual Conference on Decision and Control, CDC 2014 |
|---|---|
| Country/Territory | United States |
| City | Los Angeles |
| Period | 15/12/14 → 17/12/14 |
Bibliographical note
Publisher Copyright:© 2014 IEEE.