Propellant sloshing torque H - Based observer design for enhanced attitude control

Anthony Bourdelle, Jean Marc Biannic, Helene Evain, Sabine Moreno, Christelle Pittet, Laurent Burlion

Research output: Contribution to journalConference articlepeer-review

Abstract

In this paper a control-oriented LPV model of the sloshing torque arising during attitude maneuvers, supported by Computational Fluid Dynamics results, is presented and used for attitude control design. The proposed strategy essentially relies on the design of a robust LPV-based disturbance torque observer with the help of the structured multi-model H synthesis framework. The estimated torque is then used to improve a satisfying attitude controller initially designed without sloshing. The stability of the parameter-varying closed-loop system is finally proved with quadratic Lyapunov functions.

Original languageEnglish (US)
Pages (from-to)286-291
Number of pages6
JournalIFAC-PapersOnLine
Volume52
Issue number12
DOIs
StatePublished - Oct 2019
Event21st IFAC Symposium on Automatic Control in Aerospace, ACA 2019 - Cranfield, United Kingdom
Duration: Aug 27 2019Aug 30 2019

All Science Journal Classification (ASJC) codes

  • Control and Systems Engineering

Keywords

  • Attitude control
  • H control
  • LPV observers
  • Sloshing

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