Slosh Observer Design for Aeroelastic Launch Vehicles
Author:
Affiliation:
1. Delft University of Technology
Publisher
American Institute of Aeronautics and Astronautics
Reference24 articles.
1. DYNAMIC MODELING UNCERTAINTY AFFECTING CONTROL SYSTEM DESIGN
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1. Cascade nonlinear observer design for large amplitude of slosh variables in spacecraft maneuver with liquid propellant tank;Acta Astronautica;2023-12
2. Nonlinear Robust Control and Observation for Aeroelastic Launch Vehicles with Propellant Slosh in a Turbulent Atmosphere;AIAA SCITECH 2023 Forum;2023-01-19
3. Experimental Study on Slosh Dynamics Estimation in a Partially Filled Liquid Container Using a Low-Cost Measurement System;IEEE Sensors Journal;2022-08-15
4. Incremental Sliding Mode Control for Aeroelastic Launch Vehicles with Propellant Slosh;AIAA Scitech 2021 Forum;2021-01-04
5. Robust Control of a Conventional Aeroelastic Launch Vehicle;AIAA Scitech 2020 Forum;2020-01-05
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