Comparison of Optimal and Bioinspired Adaptive Control Laws for Spacecraft Sloshing Dynamics
Author:
Affiliation:
1. Embry-Riddle Aeronautical University, Daytona Beach, Florida 32114
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Reference25 articles.
1. Dynamic modelling and stability parametric analysis of a flexible spacecraft with fuel slosh
2. A CFD Approach to Modeling Spacecraft Fuel Slosh
3. Design of Satellite Attitude Control System Considering the Interaction between Fuel Slosh and Flexible Dynamics during the System Parameters Estimation
4. Modelling and Control of Space Vehicles with Fuel Slosh Dynamics
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2. A Moving-Horizon Estimator of the Unmeasured States for Fuel Sloshing Dynamics in Close Proximity Operation;2023 3rd International Conference on Computing and Information Technology (ICCIT);2023-09-13
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4. Distributed Intelligent Adaptive Controller for Disturbance Rejection in Multiagent Systems;Journal of Aerospace Information Systems;2023-05
5. Observer-Based Adaptive Backstepping Sliding-Mode Control of the Satellite Attitude with a Partially Filled Spherical Fuel Tank;Iranian Journal of Science and Technology, Transactions of Mechanical Engineering;2023-01-02
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