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) |
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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 |
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Country/Territory | United States |
City | Minneapolis, MN |
Period | 6/14/06 → 6/16/06 |
ASJC Scopus subject areas
- Electrical and Electronic Engineering