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A Precise and GNSS-Free Landing System on Moving Platforms for Rotary-Wing UAVs
Francisco Alarcón1, Manuel García2, Ivan Maza3
1Center for Advanced Aerospace Technologies, Calle Wilbur y Orville Wright, 19, La Rinconada, 41300 Sevilla, Spain. falarcon@catec.aero.
This study introduces a novel cable-based system for precise, centimeter-accurate landings of unmanned rotorcraft on moving platforms. The system enhances safety and stability without relying on Global Navigation Satellite Systems (GNSS).
Area of Science:
- Robotics
- Aerospace Engineering
- Control Systems
Background:
- Global Navigation Satellite System (GNSS)-denied environments pose challenges for Unmanned Aerial Vehicle (UAV) operations.
- Precise landing on dynamic platforms is critical for many UAV applications, including maritime operations and logistics.
Purpose of the Study:
- To develop and validate a novel landing system for rotary-wing UAVs that achieves centimeter-level accuracy on moving platforms.
- To demonstrate a GNSS-independent approach for safe and robust UAV landings.
Main Methods:
- A physical cable connecting the UAV and the landing platform was used to derive relative position and velocity.
- The system utilizes angles from the cable to calculate state information, enhancing altitude control and stability.
- The developed system was implemented on an unmanned helicopter for extensive testing.
Main Results:
- Achieved centimeter-level landing accuracy using only local sensors, without GNSS.
- Demonstrated robustness across various test conditions and platform trajectories.
- The system enabled the helicopter to accurately follow the moving landing platform at different velocities.
Conclusions:
- The proposed cable-based system offers a precise, robust, and GNSS-independent solution for UAV landings on moving platforms.
- The system provides enhanced control over UAV altitude, centering, and post-contact stability.
- This technology significantly advances the capabilities of rotary-wing UAVs in challenging operational environments.
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