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This research applies machine learning techniques specifically designed to preserve differential flatness in multi-quadrotor systems, enabling high-fidelity aerodynamic compensation within compute-constrained flight stacks. By using a physics-informed residual dynamics framework, the approach achieves tracking performance comparable to complex nonlinear model predictive control while requiring significantly less computational power and minimal training data. The work represents a meaningful advancement at the intersection of machine learning and robotics control theory rather than general consumer electronics or networking standards.
Flatness-Preserving Residual Learning for Real-Time Tight Quadrotor Formation Flight
arXiv:2607.12275v2 Announce Type: replace Abstract: Quadrotors flying in tight formations are severely affected by turbulent aerodynamic interactions, such as downwash, that can cause catastrophic collisions if left unmodeled. To compensate for these effects, we propose a physics-informed residual dynamics learning framework that captures complex aerodynamic interactions while ensuring the joint multi-quadrotor system remains differentially flat. We leverage this preserved flatness to design a computationally efficient feedback linearization controller that is easily tunable with linear control techniques and cancels aerodynamic disturbances via feedforward compensation. Hardware experiments demonstrate our framework reduces average tracking errors by 31% compared to nominal baselines. Crucially, our lightweight approach matches the tracking performance of state-of-the-art nonlinear model predictive control (NMPC) while requiring an order of magnitude less computation. We are the first to show that stable, tight formation flight can be achieved with under 30 seconds of training data and a 5ms loop rate, unlocking high-fidelity aerodynamic compensation for compute-constrained flight stacks.
Abstract:Quadrotors flying in tight formations are severely affected by turbulent aerodynamic interactions, such as downwash, that can cause catastrophic collisions if left unmodeled. To compensate for these effects, we propose a physics-informed residual dynamics learning framework that captures complex aerodynamic interactions while ensuring the joint multi-quadrotor system remains differentially flat. We leverage this preserved flatness to design a computationally efficient feedback linearization controller that is easily tunable with linear control techniques and cancels aerodynamic disturbances via feedforward compensation. Hardware experiments demonstrate our framework reduces average tracking errors by 31% compared to nominal baselines. Crucially, our lightweight approach matches the tracking performance of state-of-the-art nonlinear model predictive control (NMPC) while requiring an order of magnitude less computation. We are the first to show that stable, tight formation flight can be achieved with under 30 seconds of training data and a 5ms loop rate, unlocking high-fidelity aerodynamic compensation for compute-constrained flight stacks.
Robotics (cs.RO); Systems and Control (eess.SY)
arXiv:2607.12275 [cs.RO]
(or arXiv:2607.12275v2 [cs.RO] for this version)
https://doi.org/10.48550/arXiv.2607.12275 Focus to learn more arXiv-issued DOI via DataCite
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