Robust Pitch Attitude Hold with MRAC for a Nonlinear Light Combat Aircraft Model
D. Wagner, M. Hromčík
Czech Technical University in Prague
Abstract
In this paper, we implement a robust model reference adaptive control (MRAC) as part of an ongoing effort to demonstrate practical application of a nonlinear control system to the pitch -attitude hold of an aircraft model. We show that MRAC can improve transient performance and compensate changes in the performance characteristics of the aircraft mid-flight by evaluating an example where a change in center of gravity of the aircraft is coupled with decreased control effectiveness.
Full paper
Session
Robust and Adaptive Control (Lecture)
Reference
Wagner, D.; Hromčík, M.: Robust Pitch Attitude Hold with MRAC for a Nonlinear Light Combat Aircraft Model. Editors: Fikar, M. and Kvasnica, M., In Proceedings of the 2017 21st International Conference on Process Control (PC), Štrbské Pleso, Slovakia, June 6 – 9, 71–75, 2017.
BibTeX
| @inProceedings{pc2017-041, | ||
| author | = { | Wagner, D. and Hrom\v{c}\'ik, M.}, |
| title | = { | Robust Pitch Attitude Hold with MRAC for a Nonlinear Light Combat Aircraft Model}, |
| booktitle | = { | Proceedings of the 2017 21st International Conference on Process Control (PC)}, |
| year | = { | 2017}, |
| pages | = { | 71-75}, |
| editor | = { | Fikar, M. and Kvasnica, M.}, |
| address | = { | \v{S}trbsk\'e Pleso, Slovakia}} |