Software-in-the-Loop Validation of a Novel Two-Point Optimal Guidance for Perturbed Spacecraft Rendezvous and Formations
Author:
Publisher
Springer Science and Business Media LLC
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://link.springer.com/content/pdf/10.1007/s40295-023-00405-8.pdf
Reference36 articles.
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3. Chen, C.T.: Linear system theory and design. Oxford University Press, Oxford (1999)
4. Chihabi, Y., Ulrich, S.: Hybrid guardian map-based adaptive control of spacecraft formation flying on highly elliptical orbits in the restricted three-body problem. Acta Astronaut. 180, 370–385 (2021). https://doi.org/10.1016/j.actaastro.2020.12.048
5. Chihabi, Y., Ulrich, S.: Linear time-varying state transition matrix for spacecraft relative dynamics on highly elliptical orbits. Acta Astronaut. 198, 208–224 (2022). https://doi.org/10.1016/j.actaastro.2022.05.056
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