Nonlinear Feedforward and Reference Systems for Adaptive Flight Control
(2013) 2013 AIAA Guidance, Navigation, and Control Conference- Abstract
- Use of feedforward can alleviate feedback and adaptive actions. Feedforward signals can be generated from reference models and the same models can also be used as reference models in adaptive control. A method for designing the reference models is presented in the paper. By exploiting the structure of the equations describing air vehicles it is possible to find reference models that scale to the present flight condition and vehicle configuration. Such reference systems are derived for flying vehicles in a generic manner, suitable for both
winged aircraft and missiles. The same type of reference systems are also used to create trajectories for feedforward signals that compensate known plant non-linearities.
Please use this url to cite or link to this publication:
https://lup.lub.lu.se/record/3994063
- author
- Pettersson, Anders LU ; Åström, Karl Johan LU ; Robertsson, Anders LU and Johansson, Rolf LU
- organization
- publishing date
- 2013
- type
- Chapter in Book/Report/Conference proceeding
- publication status
- published
- subject
- host publication
- 2013 AIAA Guidance, Navigation, and Control Conference
- pages
- 19 pages
- conference name
- 2013 AIAA Guidance, Navigation, and Control Conference
- conference location
- Boston, MA, United States
- conference dates
- 2013-08-19
- external identifiers
-
- scopus:84883699089
- DOI
- 10.2514/6.2013-5001
- project
- NFFP5 Adaptive Control in Flying Vehicles
- language
- English
- LU publication?
- yes
- id
- 10c117c3-6265-4a28-afe6-a9afe5ff0ad4 (old id 3994063)
- date added to LUP
- 2016-04-04 14:37:07
- date last changed
- 2024-01-04 00:35:36
@inproceedings{10c117c3-6265-4a28-afe6-a9afe5ff0ad4, abstract = {{Use of feedforward can alleviate feedback and adaptive actions. Feedforward signals can be generated from reference models and the same models can also be used as reference models in adaptive control. A method for designing the reference models is presented in the paper. By exploiting the structure of the equations describing air vehicles it is possible to find reference models that scale to the present flight condition and vehicle configuration. Such reference systems are derived for flying vehicles in a generic manner, suitable for both<br/><br> winged aircraft and missiles. The same type of reference systems are also used to create trajectories for feedforward signals that compensate known plant non-linearities.}}, author = {{Pettersson, Anders and Åström, Karl Johan and Robertsson, Anders and Johansson, Rolf}}, booktitle = {{2013 AIAA Guidance, Navigation, and Control Conference}}, language = {{eng}}, title = {{Nonlinear Feedforward and Reference Systems for Adaptive Flight Control}}, url = {{https://lup.lub.lu.se/search/files/6402072/4003265.pdf}}, doi = {{10.2514/6.2013-5001}}, year = {{2013}}, }