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A Dual Quaternion Based Visual Odometry Method for a Lunar Lander
Date
2024-01-01
Author
Uzun, Semra Sultan
Söken, Halil Ersin
Metadata
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Visual sensors have a major advantage over traditional sensing methods for navigation in unknown environments since they provide rich information about the environment. However, they do not offer direct navigation measurements, and the images must be pre-processed. To extract meaningful information, the development of reliable and computationally efficient algorithms are required. This study presents a visual odometry solution that can effectively operate to estimate the pose of a small lander for the soft moon landing. For this purpose, an algorithm is designed to estimate the angular and translational velocities of the spacecraft during the descent and landing phases. A Kalman filter-based algorithm is proposed, which uses the dual quaternion formulation to provide a linear Kalman filter for velocity estimation. The proposed algorithm is tested in a simulation environment for a lunar landing scenario.
URI
https://www.scopus.com/inward/record.uri?partnerID=HzOxMe3b&scp=85193836953&origin=inward
https://hdl.handle.net/11511/109904
DOI
https://doi.org/10.1109/aero58975.2024.10521187
Conference Name
2024 IEEE Aerospace Conference, AERO 2024
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Department of Aerospace Engineering, Conference / Seminar
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BibTeX
S. S. Uzun and H. E. Söken, “A Dual Quaternion Based Visual Odometry Method for a Lunar Lander,” presented at the 2024 IEEE Aerospace Conference, AERO 2024, Montana, Amerika Birleşik Devletleri, 2024, Accessed: 00, 2024. [Online]. Available: https://www.scopus.com/inward/record.uri?partnerID=HzOxMe3b&scp=85193836953&origin=inward.