Jun Shi |
Research Associate, Technical University of Munich, Institute of Flight System Dynamics, 85748, Garching, Germany. | Xiang Fang |
Research Associate, Technical University of Munich, Institute of Flight System Dynamics, 85748, Garching, Germany. | Nils Schlautmann |
Research Associate, Technical University of Munich, Institute of Flight System Dynamics, 85748, Garching, Germany. | Michael Zintl |
Research Associate, Technical University of Munich, Institute of Flight System Dynamics, 85748, Garching, Germany. | Johann Dambeck |
Professor, Technical University of Munich, Institute of Flight System Dynamics, 85748, Garching, Germany. | Florian Holzapfel |
Professor, Technical University of Munich, Institute of Flight System Dynamics, 85748, Garching, Germany. |
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Abstract:
Automatic landing of VTOL aircraft under low illumination conditions, e.g., night operations, is challenging. To address this challenge, this paper proposes a novel design of ground-based infrastructure comprising a landing pad equipped with optical markers including finder markers and active markers. The design enables a VTOL aircraft equipped with an onboard camera to obtain real-time 6-degree-of-freedom relative pose during the landing phase under low illumination conditions since the optical markers are composed of active light sources. The well-structured layout geometry of the finder markers facilitates robust landing pad detection from aerial images without relying on complicated feature-matching technology. The active markers, employing specific blinking frequencies, contribute to the unique identification of the landing pad, ensuring a secure landing. To validate the feasibility of relative pose estimation with the proposed layout of optical markers, a modified four-point algorithm is applied for pose estimation in this paper. Compared with the classic four-point algorithm, our solution avoids the explicit ambiguity resolution. It uniquely determines the relative pose by fully leveraging prior knowledge of the landing pad surface. Simulations with a landing trajectory demonstrate that the proposed landing pad design is theoretically feasible for automatic take-off and landing in terms of recognition and pose estimation.
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