Attitude guidance and tracking for spacecraft with two reaction wheels
Author:
Affiliation:
1. Department of Aerospace Science and Technology, Politecnico di Milano, Milano, Italy
2. School of Astronautics, Harbin Institute of Technology, Harbin, P.R. China
Publisher
Informa UK Limited
Subject
Computer Science Applications,Control and Systems Engineering
Link
https://www.tandfonline.com/doi/pdf/10.1080/00207179.2017.1299944
Reference20 articles.
1. A topological obstruction to continuous global stabilization of rotational motion and the unwinding phenomenon
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3. Geometric Attitude Motion Planning for Spacecraft with Pointing and Actuator Constraints
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5. Adaptive Fault-Tolerant Control of Spacecraft Attitude Dynamics with Actuator Failures
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