Consensus Control of Rigid Body Spacecraft in Orbital Relative Motion using TSE(3) and Exponential Coordinates
Author:
Publisher
Springer Science and Business Media LLC
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://link.springer.com/content/pdf/10.1007/s40295-022-00322-2.pdf
Reference28 articles.
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2. Sarlette, A., Sepulchre, R., Leonard, N.E.: Autonomous rigid body attitude synchronization. Automatica 45(2), 572–577 (2009)
3. Maadani, M., Butcher, E.A., Nazari, M., Yucelen, T.: Decentralized consensus control of rigid bodies using exponential coordinates. In: AIAA Scitech 2019 Forum, p. 1161 (2019)
4. Maadani, M., Butcher, E.A., Sanyal, A.K.: Finite-time attitude consensus control of a multi-agent rigid body system. In: American Control Conference (ACC), IEEE, 2020, pp 877–882 (2020)
5. Zou, Y., Meng, Z.: Velocity-free leader–follower cooperative attitude tracking of multiple rigid bodies on SO(3). IEEE Trans. Cybern. 49(12), 4078–4089 (2018)
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2. Relative Spacecraft Position and Attitude in the Circular Restricted Three-Body Problem: TSE(3) vs. Dual Quaternions;AIAA SCITECH 2023 Forum;2023-01-19
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