Resilient structured periodic H2 synthesis for a spacecraft in elliptical orbits

Abstract : Station-keeping of a small spacecraft is studied and a solution based on resilient periodic state-feedback control laws is proposed. Linearized equations of the relative motion of the satellite near an eccentric reference orbit are derived in the presence of the second zonal gravitational harmonic J2 and atmospheric drag perturbations. After a discretization of the model, a resilient H2 state-feedback control law is computed by a linear matrix inequality-based algorithm. Illustrative non linear simulations show the efficiency of the approach.
Document type :
Conference papers
Liste complète des métadonnées

https://hal.archives-ouvertes.fr/hal-00331208
Contributor : Christophe Farges <>
Submitted on : Wednesday, October 15, 2008 - 4:46:34 PM
Last modification on : Friday, April 12, 2019 - 4:23:37 PM

Identifiers

Citation

Christophe Farges, Dimitri Peaucelle, Alain Théron, Denis Arzelier. Resilient structured periodic H2 synthesis for a spacecraft in elliptical orbits. 17th IFAC Symposium on Automatic Control in Aerospace. ACA'07., Jun 2007, Toulouse, France. pp.633-638, ⟨10.3182/20070625-5-FR-2916.00108⟩. ⟨hal-00331208⟩

Share

Metrics

Record views

150