Abstract
This paper presents an adaptive disturbance rejection control architecture for a flying vehicle to track a maneuvering target using a monocular camera as a visual sensor. The derived guidance law is an acceleration command for the follower and enures range regulation with desired precision. Simulations illustrate the performance of the method.
| Original language | English (US) |
|---|---|
| Title of host publication | Proceedings of the 2006 American Control Conference |
| Pages | 2850-2855 |
| Number of pages | 6 |
| Volume | 2006 |
| State | Published - 2006 |
| Externally published | Yes |
| Event | 2006 American Control Conference - Minneapolis, MN, United States Duration: Jun 14 2006 → Jun 16 2006 |
Other
| Other | 2006 American Control Conference |
|---|---|
| Country/Territory | United States |
| City | Minneapolis, MN |
| Period | 6/14/06 → 6/16/06 |
ASJC Scopus subject areas
- Electrical and Electronic Engineering