Attitude tracking control of flexible spacecraft with large amplitude slosh
Abstract
This paper is focused on attitude tracking control of a spacecraft that is equipped with flexible appendage and partially filled liquid propellant tank. The large amplitude liquid slosh is included by using a moving pulsating ball model that is further improved to estimate the settling location of liquid in microgravity or a zero-g environment. The flexible appendage is modelled as a three-dimensional Bernoulli–Euler beam, and the assumed modal...
Paper Details
Title
Attitude tracking control of flexible spacecraft with large amplitude slosh
Published Date
Aug 1, 2017
Journal
Volume
33
Issue
6
Pages
1095 - 1102
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