Cascade nonlinear observer design for large amplitude of slosh variables in spacecraft maneuver with liquid propellant tank-Reference-Cited by-同舟云学术

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Cascade nonlinear observer design for large amplitude of slosh variables in spacecraft maneuver with liquid propellant tank

Published:2023-12 Issue: Volume:213 Page:35-48
ISSN:0094-5765
Container-title:Acta Astronautica
language:en
Short-container-title:Acta Astronautica

Author:

Park Jooho^ORCID,Bang Hyochoong^ORCID,Park Kyun-Sang^ORCID,Lee Seon-Ho

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference45 articles.

1. Spacecraft Dynamics and Control: a Practical Engineering Approach, Vol. 7;Sidi,1997

2. Liquid Sloshing Dynamics: Theory and Applications;Ibrahim,2005

3. J. Pei, P.M. Rothhaar, Demonstration of launch vehicle slosh instability on a pole-cart platform, in: AIAA Atmospheric Flight Mechanics Conference, 2015, p. 2712.

4. Advanced GNC-oriented modeling and simulation of vertical landing vehicles with fuel slosh dynamics;Farì;Acta Astronaut.,2023

5. Behavior of Spinning Space Vehicles with Onboard Liquids;Hubert,2008

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