Journal article
Optimal trajectory tracking using an output feedback preview controller
- Abstract:
- This paper investigates the use of preview control for optimal trajectory tracking for air-to-surface missiles. An off-line reference trajectory is obtained by solving a trajectory optimisation problem that incorporates the mission constraints. A trajectory following guidance scheme using a preview controller is used to generate the on-line control. An example of a terminal guidance trajectory with a bunt (climb and dive) manoeuvre and a look angle constraint is presented to demonstrate the method. © MBDA UK Ltd.
Actions
Access Document
- Publisher copy:
- 10.1049/ic:20060560
Authors
- Journal:
- IET Seminar Digest More from this journal
- Volume:
- 2006
- Issue:
- 11359
- Pages:
- 97-104
- Publication date:
- 2006-01-01
- DOI:
- Language:
-
English
- Pubs id:
-
pubs:367587
- UUID:
-
uuid:10edace9-d90f-4ffe-8d99-d22b1729bbcc
- Local pid:
-
pubs:367587
- Source identifiers:
-
367587
- Deposit date:
-
2013-11-17
- ARK identifier:
Terms of use
- Copyright date:
- 2006
If you are the owner of this record, you can report an update to it here: Report update to this record