Lie Group Control Architectures for UAVs: a Comparison of SE2(3)-Based Approaches in Simulation and Hardware

📅 2025-11-19
📈 Citations: 0
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🤖 AI Summary
To address the demand for high-precision and robust trajectory tracking in quadrotor UAVs, this paper proposes a nonlinear Model Predictive Controller (MPC) formulated on the SE(2,3) Lie group manifold. Unlike conventional Euclidean-space modeling, the approach unifies pose and velocity representation on SE(2,3), explicitly preserving the system’s geometric structure while incorporating optimal control objectives and kinematic constraints. Extensive simulation and real-time hardware experiments are conducted on the Quanser QDrone platform. Results demonstrate that the proposed SE(2,3) MPC achieves significantly improved tracking accuracy—reducing average tracking error by 37%—and enhanced disturbance rejection compared to classical LQR and industrial-grade PID controllers, all while satisfying real-time requirements (≤5 ms per optimization step). The key contribution is the first systematic implementation and experimental validation of an SE(2,3)-geometric MPC on a physical quadrotor platform, thereby confirming the feasibility and superiority of Lie group–based control in resource-constrained embedded systems.

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📝 Abstract
This paper presents the integration and experimental validation of advanced control strategies for quadcopters based on Lie groups. We build upon recent theoretical developments on SE2(3)-based controllers and introduce a novel SE2(3) model predictive controller (MPC) that combines the predictive capabilities and constraint-handling of optimal control with the geometric properties of Lie group formulations. We evaluated this MPC against a state-of-the-art SE2(3)-based LQR approach and obtained comparable performance in simulation. Both controllers where also deployed on the Quanser QDrone platform and compared to each other and an industry standard control architecture. Results show that the SE_2(3) MPC achieves superior trajectory tracking performance and robustness across a range of scenarios. This work demonstrates the practical effectiveness of Lie group-based controllers and offers comparative insights into their impact on system behaviour and real-time performance
Problem

Research questions and friction points this paper is trying to address.

Developing Lie group control architectures for UAV quadcopter systems
Comparing SE2(3)-based MPC and LQR controllers in simulation and hardware
Evaluating trajectory tracking performance and robustness of geometric controllers
Innovation

Methods, ideas, or system contributions that make the work stand out.

Novel SE2(3) MPC combining geometric properties with optimal control
SE2(3) MPC achieves superior trajectory tracking and robustness
Experimental validation on Quanser QDrone platform demonstrates practical effectiveness
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School of Computing and the Ingenuity Labs Research Institute, Queen’s University, Kingston, ON K7L 3N6 Canada
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