Attitude tracking control of a flexible spacecraft under angular velocity constraints

Laurent Burlion, Jean Marc Biannic, Tarek Ahmed-Ali

Research output: Contribution to journalArticlepeer-review

3 Scopus citations

Abstract

In this paper, a new technique is proposed for trajectory tracking of a flexible spacecraft subject to angular velocity constraints. The problem is addressed using an output to input saturation transformation (OIST) which converts the prescribed bounds into state-dependent saturations on the control input signals. It is shown that an interval observer can be used in combination with the OIST technique to ensure that the constraints remain satisfied despite unmeasured flexible modes and torque disturbances. Some realistic simulations conclude the paper and validate our approach.

Original languageEnglish (US)
Pages (from-to)1524-1540
Number of pages17
JournalInternational Journal of Control
Volume92
Issue number7
DOIs
StatePublished - Jul 3 2019
Externally publishedYes

All Science Journal Classification (ASJC) codes

  • Control and Systems Engineering
  • Computer Science Applications

Keywords

  • Constrained control
  • anti-windup
  • attitude stabilisation
  • interval observers
  • spacecraft
  • time-domain constraint

Fingerprint

Dive into the research topics of 'Attitude tracking control of a flexible spacecraft under angular velocity constraints'. Together they form a unique fingerprint.

Cite this