Embedding a SDP-based control algorithm for the orbital rendezvous hovering phases

In this paper we present the procedures for embedding a semidefinite programming-based control algorithm for the impulsive rendezvous hovering phases problem on a board containing a synthesized LEON3 microprocessor. The performance of this algorithm is benchmarked by means of simulations against traditional linear programming-based constraint discretization approaches.

Keywords

FPGA embedded control law semidefinite programming optimization-based control polynomial non-negativity aerospace impulsive rendezvous

Domains

Optimization and Control [math.OC] Automatic

Fichier principal

ICINS_2018_HAL.pdf (762.79 Ko)

Origin	Files produced by the author(s)

Paulo Ricardo Arantes Gilz : Connect in order to contact the contributor

https://laas.hal.science/hal-01729956

Submitted on : Tuesday, March 13, 2018-5:04:06 PM

Last modification on : Monday, April 8, 2024-2:04:09 PM

Long-term archiving on: Thursday, June 14, 2018-12:20:37 PM

Dates and versions

hal-01729956 , version 1 (13-03-2018)

Identifiers

HAL Id : hal-01729956 , version 1

Cite

Frédéric Camps, Paulo Ricardo Arantes Gilz, Mioara Joldes, Christophe Louembet. Embedding a SDP-based control algorithm for the orbital rendezvous hovering phases. International Conference on Integrated Navigation Systems (ICINS 2018), May 2018, Saint Petersburg, Russia. 10p. ⟨hal-01729956⟩

Export

BibTeX XML-TEI Dublin Core DC Terms EndNote DataCite

Collections

UNIV-TLSE2 CNRS INSA-TOULOUSE LAAS LAAS-MAC UT1-CAPITOLE LAAS-IDEA LAAS-DECISION-ET-OPTIMISATION TDS-MACS INSA-GROUPE ANR TOULOUSE-INP UNIV-UT3 UT3-TOULOUSEINP

118 View

40 Download