Research
Flatness-Preserving Residual Learning for Real-Time Tight Quadrotor Formation Flight
arXiv:2607.12275v1 Announce Type: new Abstract: Quadrotors flying in tight formations are severely affected by turbulent aerodynamic interactions, such as downwash, that can cause catastrophic collisi
arXiv:2607.12275v1 Announce Type: new 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.
Related
- Leaderless Collective Motion in Affine Formation Control over the Complex Plane
- Topological Online Learning for Displacement-based Formation Control
- Learned Incremental Nonlinear Dynamic Inversion for Quadrotors with and without Slung Payloads
- AcroRL: Learning Aggressive Quadrotor Inversion using Bidirectional Thrust
- Realtime Wind Estimation using Low Cost Quadrotor Uncrewed Aerial Vehicles
Source: arXiv cs.RO | 2026-07-15