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  4. A velocity qLMPC algorithm for path-following with obstacle avoidance for fixed-wing UAVs
 
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A velocity qLMPC algorithm for path-following with obstacle avoidance for fixed-wing UAVs

Publikationstyp
Conference Paper
Date Issued
2024-01-01
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  
Rieck, Leif Alexander  
Flugzeug-Systemtechnik M-7  
Thielecke, Frank  
Flugzeug-Systemtechnik M-7  
TORE-URI
https://hdl.handle.net/11420/48444
Start Page
107
End Page
112
Citation
2024 International Conference on Unmanned Aircraft Systems, ICUAS 2024
Contribution to Conference
2024 International Conference on Unmanned Aircraft Systems, ICUAS 2024  
Publisher DOI
10.1109/ICUAS60882.2024.10557102
Scopus ID
2-s2.0-85197396438
Publisher
IEEE
ISBN
9798350357882
This paper tackles the problem of path-following control for fixed-wing unmanned aerial vehicles (UAVs), while accounting for wind disturbances and hindering obstacles. We introduce a novel predictive algorithm based on a quasi-linear parameter-varying (qLPV) model representation of the 3D kinematics of the fixed-wing aircraft. This approach allows us to utilize efficient Quadratic Programming (QP) solvers to find efficient and fast solutions to the Optimal Control Problem (OCP), typically within milliseconds. Additionally, it facilitates the incorporation of appropriate constraints aligned with the aircraft dynamics and obstacle constraints after further processing. In this paper, we demonstrate how the nonlinear obstacle constraints can also be represented in a qLPV form, making it feasible to handle them within our framework. Moreover, stability conditions can be directly derived based on the qLPV representation. The algorithm's effectiveness is demonstrated on an aerobatic unmanned aircraft with a successive-loop-closure (SLC) based attitude and stabilization controller. The evaluation is conducted across two scenarios previously used in experimental flights with the same aircraft. Each scenario involves nine waypoints, obstructive obstacles, and wind disturbances. The simulations begin with the kinematic model and are subsequently extended to a high-fidelity model of the UAV, resulting in successful path-following and obstacle avoidance with relatively low computational times.
Subjects
Aircraft control
Antennas
Kinematics
Optimal control systems
Quadratic programming
Three dimensional computer graphics
Unmanned aerial vehicles (UAV)
DDC Class
690: Building, Construction
005: Computer Programming, Programs, Data and Security
620.1: Engineering Mechanics and Materials Science
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