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  4. Predictive Path Following Control for Fixed Wing UAVs Using the qLMPC Framework in the Presence of Wind Disturbances
 
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Predictive Path Following Control for Fixed Wing UAVs Using the qLMPC Framework in the Presence of Wind Disturbances

Publikationstyp
Conference Presentation
Date Issued
2024-01
Sprache
English
Author(s)
Samir Said Metwalli Rezk, Ahmed 
Regelungstechnik E-14  
Martínez Calderón, Horacio  
Werner, Herbert  
Regelungstechnik E-14  
Herrmann, Benjamin  orcid-logo
Flugzeug-Systemtechnik M-7  
Thielecke, Frank  
Flugzeug-Systemtechnik M-7  
TORE-URI
https://hdl.handle.net/11420/47682
Citation
AIAA SCITECH (2024)
Contribution to Conference
AIAA SCITECH 2024
Publisher DOI
10.2514/6.2024-1594
Scopus ID
2-s2.0-85194188835
Publisher
American Institute of Aeronautics and Astronautics
This paper presents a cascaded approach for a predictive path-following scheme using quasi-linear parameter-varying model predictive control (qLMPC) applied to a 25 kg unmanned aerobatic aircraft. The quasi-linear parameter-varying (qLPV) representation provides a semi-linear model of the nonlinear system, while fast solvers are utilized to solve quadratic optimization problems (QOPs) in milliseconds. To incorporate integral action and overcome wind disturbances, a velocity-based linearization of the model is employed. Two scenarios with nine waypoints each are evaluated using a hybrid strategy that combines arc-length parameterization with cubic splines and a synthetic waypoint path-planner. The path-following strategy is applied to both simplified kinematic and high-fidelity models of the aircraft, with constant wind in the first scenario and time-varying wind in the second scenario. The algorithm achieves good performance in both scenarios with short computation times. Lastly, a performance analysis of the strategy with the two path-planning techniques is presented.
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