Observer-Based Robust Attitude Control of Liquid-Filled Flexible Spacecraft in a Fully Actuated System Framework
Author:
Affiliation:
1. Harbin Institute of Technology
Publisher
American Society of Civil Engineers (ASCE)
Link
https://ascelibrary.org/doi/pdf/10.1061/JAEEEZ.ASENG-5294
Reference73 articles.
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2. A topological obstruction to continuous global stabilization of rotational motion and the unwinding phenomenon
3. Multi-observer approach for tracking control of flexible spacecraft using exponential mapping of SE(3)
4. Chen Y. P. and S. C. Lo. 1993. “Sliding-mode controller design for spacecraft attitude tracking maneuvers.” In Proc. American Control Conf. 195–196. New York: IEEE.
5. Integrated vibration suppression attitude control for flexible spacecrafts with internal liquid sloshing
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