Low-Latency Quasi-Static Modeling of UAV Tether Aerodynamics
Max Beffert, Andreas Zell

TL;DR
This paper introduces two low-latency quasi-static tether modeling methods with aerodynamics for UAVs, enabling real-time simulation and control in dynamic conditions.
Contribution
It presents an analytical and a numerical approach for fast, accurate tether force modeling with aerodynamic effects, validated through real-world tests.
Findings
Analytical method solves in under 1 ms with sufficient accuracy.
Numerical method achieves 5 ms solve time with higher flexibility.
Both methods are validated with real-world tether force measurements.
Abstract
One of the main limitations of multirotor UAVs is their short flight time due to battery constraints. A practical solution for continuous operation is to power the drone from the ground via a tether. While this approach has been demonstrated for stationary systems, scenarios with a fast-moving base vehicle or strong wind conditions require modeling the tether forces, including aerodynamic effects. In this work, we propose two complementary approaches for low-latency quasi-static tether modeling with aerodynamics. The first is an analytical method based on catenary theory with a uniform drag assumption, achieving very fast solve times below 1 ms. The second is a numerical method that discretizes the tether into segments and lumped masses, solving the equilibrium equations using CasADi and IPOPT. By leveraging initialization strategies, such as warm starting and analytical initialization,…
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