ATTITUDE CONTROL SYSTEM DESIGN FOR A RIGID-FLEXIBLE SATELLITE USING THE H-INFINITY METHOD WITH PARAMETRIC UNCERTAINTY. Revista Interdisciplinar de Pesquisa em Engenharia, [S. l.], v. 2, n. 19, p. 84–90, 2017. DOI: 10.26512/ripe.v2i19.15022. Disponível em: https://periodicostestes.bce.unb.br/index.php/ripe/article/view/15022. Acesso em: 13 mar. 2025.