Abstract
This paper presents adaptive control architecture for the safe flight of a transport aircraft under adverse operating conditions and uncertainties. This architecture combines a nominal controller based on an LQR with integral action, and an adaptive controller that accommodates for actuator saturation and disturbances. In this paper, we consider the control of the C-5 transport aircraft, which is similar to the Generic Transport Model. We delineate the underlying nonlinear dynamic model and introduce various upsets, damages, and failures by representing these various adverse conditions in the form of uncertainties.
Original language | English |
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Title of host publication | Mechatronics and Intelligent Materials II |
Pages | 105-109 |
Number of pages | 5 |
DOIs | |
Publication status | Published - 2012 |
Event | 2nd International Conference on Mechatronics and Intelligent Materials 2012, MIM 2012 - GuiLin, China Duration: 18 May 2012 → 19 May 2012 |
Publication series
Name | Advanced Materials Research |
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Volume | 490-495 |
ISSN (Print) | 1022-6680 |
Conference
Conference | 2nd International Conference on Mechatronics and Intelligent Materials 2012, MIM 2012 |
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Country/Territory | China |
City | GuiLin |
Period | 18/05/12 → 19/05/12 |
Keywords
- Adaptive control architecture
- Aircraft
- Nominal controller
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Zhang, B., & Wang, S. (2012). An aircraft adaptive control architecture based on nominal controller. In Mechatronics and Intelligent Materials II (pp. 105-109). (Advanced Materials Research; Vol. 490-495). https://doi.org/10.4028/www.scientific.net/AMR.490-495.105