Abstract
Today, technology in the field of space is developing rapidly. In this direction, the scope and importance of studies in space is gradually expanding. Expanding space studies have created high spacecraft capabilities and precision operational processing requirements, creating the curiosity of reaching other planets and objects. In this context, rendezvous and docking problems have emerged. In this study, the docking problem was tried to be solved for two objects moving in the same orbit, and the amount of thrust required for docking was calculated using a global navigation satellite system (GNSS)-based system. With this study, the basic logic for the solutions and simulations of more complex problems to be created in the future has been tried to be examined.
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Abbreviations
- CW:
-
Clohessy-Wiltshire
- EKF:
-
Extended Kalman filter
- GNSS:
-
Global navigation satellite system
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Sever, M., Erkeç, T.Y. (2023). Rendezvous and Docking for Space Vehicles. In: Karakoc, T.H., Le Clainche, S., Chen, X., Dalkiran, A., Ercan, A.H. (eds) New Technologies and Developments in Unmanned Systems. ISUDEF 2022. Sustainable Aviation. Springer, Cham. https://doi.org/10.1007/978-3-031-37160-8_13
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DOI: https://doi.org/10.1007/978-3-031-37160-8_13
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